1965 October 1 - -
NASA formally accepted Apollo spacecraft 002 Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. At a Customer Acceptance Readiness Review at North American, NASA formally accepted spacecraft 002. The vehicle was then demated and shipped to White Sands. References: 16.
1965 October 1 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: RT-1. LV Configuration: RT-1 RT-1-1963. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi). References: 2.
1965 October 1 - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 459. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1965 October 1 - Launch Site: Baikonur. Launch Complex: PU31. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 October 1 - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: IIAE Orion. Model: Orion-1. LV Configuration: Orion-1 No. 1. -
Test mission Nation: Argentina. Agency: CNIE. Apogee: 90 km (55 mi). References: 2.
1965 October 1 - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena B006. -
USN B006 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1965 October - -
Stanford Research Institute study on Douglas manned orbital research laboratory (MORL). Nation: USA. Spacecraft: MORL. The Stanford Research Institute, Menlo Park, California, performed a study on a manned orbital research laboratory (MORL) for Douglas Aircraft Company, Inc., Santa Monica. Major conclusions of the study included the following: The MORL mission was highly desirable for the posture of the United States in the international community. The improvement of this position would represent, perhaps, MORL's greatest contribution to our nation.
Additional Details: Stanford Research Institute study on Douglas manned orbital research laboratory (MORL)..
1965 October - -
Douglas plan for orbital space station development . Nation: USA. Spacecraft: MORL. A plan for orbital space station development responsive to the research and development needs of a broad-based space exploration program was presented to the Deutsche Gesellschaft fur Rakententechnik und Raumfarht, Munich, Germany. The paper was prepared by Douglas Aircraft Company, Inc., Santa Monica. The main theme of the paper centered on low-Earth-Orbit applications of space stations. It suggested that the space station system would start with limited life laboratories and evolve into extended life, continuously manned space stations. In the development of the space station, four major subsystems would be required: life support, power, stabilization and control, and communications. Of these, the life support and power subsystems would require significant extensions to current technology. While touching on lunar-orbital and interplanetary missions, it was indicated that in the evolution of the space station the low-Earth-orbital missions were of primary importance because they could accommodate applications development, capability-engineering development, biomedical behavioral experiments, and scientific experiments. Polar orbits would be required for cartographic, meteorologic, geologic, and natural resources surveys. Synchronous orbits would be useful primarily for communications, allowing continuous communications without the necessity of vast ground or orbital relay networks.
1965 October 1 - 01:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.121CG. -
LPARL 1D XRT X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 148 km (91 mi). References: 2.
1965 October 1 - 03:57 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5B. -
Ionosphere / solar x-rays mission Nation: USSR. Agency: AN SSSR. Apogee: 480 km (290 mi). References: 2.
1965 October 2 - 04:22 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C ESRO S04/2 (SEO9). -
MPE Ba-13 / Grenades Aeronomy mission Nation: Europe. Agency: ESRO. Apogee: 250 km (150 mi). References: 2.
1965 October 3-9 - -
Testing of Apollo extravehicular mobility unit at Flagstaff Nation: USA. Program: Apollo. Spacecraft: A7L. The U.S. Geological Survey cooperated with Crew Systems Division (CSD) in testing the extravehicular mobility unit under simulated lunar conditions at Flagstaff, Arizona. As a result, CSD technicians determined a number of deficiencies in the thermal meteoroid garment, and recommended a number of changes to make the garment more functional and more durable, as well as better fitting and more comfortable.
References: 16.
1965 October 4 - -
Voskhod 3 Nation: USSR. Program: Voskhod. Flight: Voskhod 3, Voskhod 4, Voskhod 5, Voskhod 6. A major programme review is held on plans for Voskhod s/n 5, 6, and 7. Tsybin insists that to conduct all of the experiments requested by the Ministry of Defence will take ten spacecraft and missions, but only five have been authorised. Spacecraft s/n 5 will fly with dogs, on a biosat mission. Spacecraft s/n 6 and 7 are being completed for 15-day flights with two crew, outfitted for artificial gravity experiments and medical and military research. The readiness of the military experiments is very poor, due to the fact that in the past Malinovskiy over and over again prohibited any work on military uses of space, at least until the ideal military platform was developed. It was only on Keldysh's initiative that any preliminary work had been done at all. Kamanin replies to Tsybin that it was not the business of OKB-1 to develop military experiments; this was the concern of the Military of Defence. Yet, Kamanin admits to himself, there is no single organisation within the Ministry that is supervising this work. Later Kamanin takes Gagarin to a meeting with Vershinin and Marshal Grechko. The Marshal is unimpressed with Gagarin's understanding of the issues involved in the issue of whether the VVS or RVSN should handle manned spaceflight. Kamanin resolves not to take cosmonauts to such high-level meetings in the future. Grechko does understand finally how poorly Malinovskiy and his deputies have handled military spaceflight. But Malinovskiy, and his supporters, Marshal Rudenko, and Colonel-General Ponomaryov, will not give up in their effort to prevent the VVS from becoming the responsible organisation for military spaceflight.
References: 376.
1965 October 4 - 03:00 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-14. -
Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 299 km (185 mi). References: 2.
1965 October 4 - 07:56 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 U103-27. -
Luna 7 Nation: USSR. Program: Luna. Payload: E-6 s/n 11. Mass: 1,504 kg (3,315 lb). Class: Planetary. Type: Lunar. Spacecraft: Luna E-6. Agency: MOM. COSPAR: 1965-077A. USAF Sat Cat: 1610. Decay Date: 1965-10-07. Lunar soft landing attempt. The Luna 7 spacecraft was intended to achieve a soft landing on the Moon. However, due to premature retrofire and cutoff of the retrorockets, the spacecraft impacted the lunar surface in the Sea of Storms. References: 2, 6, 64, 296.
1965 October 5 - 00:42 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.30UI. -
M / DTR Ionosphere mission Nation: USA. Agency: NASA. Apogee: 960 km (590 mi). References: 2.
1965 October 5 - 03:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NRL NB3.184. -
Ultraviolet / x-ray astronomy mission Nation: USA. Agency: NRL. Apogee: 171 km (106 mi). References: 2.
1965 October 5 - 09:07 GMT - Launch Site: Vandenberg. Launch Complex: 576B3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 34D NB20.170 RS. -
OV1-02 Nation: USA. Payload: OV1 Dummy. Mass: 86 kg (189 lb). Class: Earth. Type: Magnetosphere. Spacecraft: OV1. Agency: USAF OAR. Perigee: 408 km (253 mi). Apogee: 2,735 km (1,699 mi). Inclination: 144.20 deg. Period: 117.60 min. COSPAR: 1965-078A. USAF Sat Cat: 1613. Radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
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NB20.170 Nation: USA. Payload: SPP 29. Spacecraft: OV1. Agency: USAF AFSC. COSPAR: 1965-078xx. USAF Sat Cat: 1613. References: 2, 279.
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OV1-02S Nation: USA. Class: Earth. Type: Magnetosphere. Spacecraft: OV1. Agency: USAF AFSC. COSPAR: 1965-078xx. USAF Sat Cat: 1613. References: 2, 279.
1965 October 5 - 09:27 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 178. -
Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi). References: 2.
1965 October 5 - 17:45 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 433 / Agena D SS-01B 1616. -
KH-4A 1025 Nation: USA. Payload: KH-4A s/n 1025 / Agena D 1616. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 202 km (125 mi). Apogee: 322 km (200 mi). Inclination: 75.10 deg. Period: 89.70 min. COSPAR: 1965-079A. USAF Sat Cat: 1615. Decay Date: 1965-10-29. KH-4A. Main cameras operated satisfactorily. References: 2, 6.
1965 October 5 - 23:21 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.202CA. -
Ionosphere / TMA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 206 km (128 mi). References: 2.
1965 October 6 - Launch Site: Vandenberg. Launch Complex: LF22. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2002. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1965 October 6 - 04:00 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8L. LV Configuration: Kappa 8L K-8L-9. -
Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 141 km (87 mi). References: 2.
1965 October 8 - -
Apollo Lunar Landing Research Vehicle flown to 91 m Nation: USA. Program: Apollo. Spacecraft: Apollo LLRV. A test model of the Lunar Landing Research Vehicle, designed to simulate lunar landings, was flown by former NASA X-15 pilot Joseph Walker to an altitude of 91 m (300 ft). Built by Bell Aerosystems Company under contract to NASA, the research craft had a jet engine that supported five-sixths of its weight. The pilot manipulated solid-fuel lift rockets that supported the remaining one-sixth, and the craft's attitude was controlled with jets of hydrogen peroxide.
References: 16.
1965 October 8 - -
Failed drop of Apollo boilerplate 6A due to braking parachute Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. A drop in the boilerplate 6A series, using flight-qualifiable earth landing system (ELS) components, failed because the braking parachute (not a part of the ELS) did not adequately stabilize the vehicle. MSC invited North American and Northrop-Ventura to Houston to explain the failure and to recommend corrective measures.
References: 16.
1965 October 9 - Launch Site: Hammaguira. Launch Complex: Brigitte. Launch Pad: -. Launch Vehicle: Diamant. Model: Saphir. LV Configuration: Saphir VE231 P3. -
Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 1,150 km (710 mi). References: 2.
1965 October 9 - Launch Site: Baikonur. Launch Complex: PU33. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 October 11 - -
Apollo AAP objectives described. Nation: USA. Spacecraft: Apollo X. In a paper presented at the American Institute of Aeronautics and Astronautics' fourth manned space flight meeting in St. Louis, AAP Director William B. Taylor described the focus and importance of the AAP. In contrast to Apollo, with its clear objective of lauding on the Moon, AAP's objectives were much less obvious. Under AAP, Taylor said, NASA planned to exploit the capabilities being developed for Apollo as a technological bridge to more extensive manned space flight missions of the 1970s and 1980s. AAP was not an end in itself, but rather a beginning to build flight experience, technology, and scientific data.
Additional Details: Apollo AAP objectives described..
1965 October 11 - Launch Site: Green River. Launch Complex: Pad 2. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena C016. -
USAF C016 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1965 October 12 - -
Parachute mortar failed during static testing Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. On August 26, the attachments for the pilot parachute mortar had failed during static testing on CM 006. The fittings had been redesigned and the test was not repeated. This test, the final one in the limit load series for the earth landing system, certified the structural interface between the CM and the earth landing system for the 009 flight.
References: 16.
1965 October 12 - 17:43 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 3-50-74. FAILURE: APU shutdown. -
X-15A Checkout mission Nation: USA. Agency: NASA/USAF. Apogee: 28 km (17 mi). Maximum Speed - 5001 kph. Maximum Altitude - 28770 m. References: 2.
1965 October 13 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5 VAO. -
VAO Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 500 km (310 mi). References: 2.
1965 October 13 - 03:13 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.151UG. -
Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 183 km (113 mi). References: 2.
1965 October 13 - 16:11 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.97GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 124 km (77 mi). References: 2.
1965 October 13 - 16:51 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.129GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 110 km (60 mi). References: 2.
1965 October 14 - 13:11 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 435 (TA4) / Agena D SS-01B 680. -
OGO 2 Nation: USA. Payload: OGO C (S-50). Mass: 507 kg (1,117 lb). Class: Earth. Type: Magnetosphere. Spacecraft: OGO. Agency: NASA GSF. Perigee: 419 km (260 mi). Apogee: 1,515 km (941 mi). Inclination: 87.40 deg. Period: 104.40 min. COSPAR: 1965-081A. USAF Sat Cat: 1620. Decay Date: 1981-09-17. OGO 2 was a large observatory instrumented with 20 experiments designed to make simultaneous, correlative observations of aurora and airglow emissions, energetic particles, magnetic field variations, ionospheric properties, etc., especially over the polar areas. Soon after achieving orbit, difficulties in maintaining earth lock with horizon scanners caused exhaustion of attitude control gas by October 23, 1965, 10 days after launch. At this time, the spacecraft entered a spin mode (about 0.11 rpm) with a large coning angle about the previously vertical axis. Five experiments became useless when the satellite went into this spin mode. Six additional experiments were degraded by this loss of attitude control. By April 1966, both batteries had failed, so subsequent observations were limited to sunlit portions of the orbit. By December 1966, only eight experiments were operational, five of which were not degraded by the spin mode operation. By April 1967, the tape recorders had malfunctioned and only one third of the recorded data could be processed. Spacecraft power and periods of operational scheduling conflicts created six large data gaps so that data were observed on a total of about 306 days of the 2-yr, 18-day total span of observed satellite data to November 1, 1967. The spacecraft was shut down on November 1, 1967, with eight experiments still operational. It was reactivated for 2 weeks in February 1968 to operate the rubidium vapor magnetometer experiment.
References: 2, 6.
1965 October 14 - 19:40 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 U103-37. -
Molniya 1-02 Nation: USSR. Program: Molniya. Payload: Molniya-1. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-1. Agency: MOM. Perigee: 487 km (302 mi). Apogee: 39,921 km (24,805 mi). Inclination: 65.20 deg. Period: 718.80 min. COSPAR: 1965-080A. USAF Sat Cat: 1621. Decay Date: 1967-03-17. France - USSR communications link. Second communications satellite 'Molniya-1'. Television programme transmission and long-range, two-way multi-channel telephone, phototelegraph and telegraph communications. References: 2, 6, 64.
1965 October 14 - 20:46 GMT - Launch Site: Delamar Dry Lake DZ. Launch Complex: -. Launch Pad: 37.3 N x 114.9 W. Launch Vehicle: X-15. LV Configuration: X-15 1-61-101. -
X-15A MIT,Pace transducer test Nation: USA. Agency: NASA/USAF. Apogee: 81 km (50 mi). Maximum Speed - 5718 kph. Maximum Altitude - 81230 m. Astronaut wings flight (USAF definition). References: 2.
1965 October 15 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ PRV. LV Configuration: HJ PRV Pacemaker. -
Apollo test re-entry vehicle test flight Nation: USA. Agency: NASA LaRC. Apogee: 23 km (14 mi). References: 2.
1965 October 15 - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. Model: Vesta. LV Configuration: Vesta 001. -
FU-123 test Nation: France. Agency: CNES. Apogee: 150 km (90 mi). References: 2.
1965 October 15 - Launch Site: Baikonur. Launch Complex: PU32. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 October 15 - Launch Site: Cape Canaveral. Launch Complex: LC40. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3C. LV Configuration: Titan IIIC 3C-4. FAILURE: Partial Failure. -
OV2-01 Nation: USA. Mass: 170 kg (370 lb). Class: Earth. Type: Magnetosphere. Spacecraft: OV2. Agency: -. Perigee: 708 km (439 mi). Apogee: 791 km (491 mi). Inclination: 32.60 deg. Period: 99.80 min. COSPAR: 1965-082B. USAF Sat Cat: 1624. Decay Date: 1972-07-27. Dual launch with LCS 2; upper stage broke up. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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Transtage 4 Nation: USA. Spacecraft: OV2. Agency: USAF. COSPAR: 1965-082xx. USAF Sat Cat: 1624. Decay Date: 1972-07-27. References: 2, 279.
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LCS 2 Nation: USA. Payload: OV2-01 / Transtage 4. Class: Calibration. Spacecraft: LCS. Agency: USAF. Perigee: 730 km (450 mi). Apogee: 785 km (487 mi). Inclination: 32.30 deg. Period: 99.98 min. COSPAR: 1965-082A. USAF Sat Cat: 1624. Decay Date: 1965-10-15. Dual launch with OV2-1; upper stage broke up. References: 2, 126.
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LCS 2 Nation: USA. Spacecraft: OV2. Agency: USAF. COSPAR: 1965-082xx. References: 2, 279.
1965 October 16 - 08:09 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. LV Configuration: Voskhod 11A57 U15001-04. -
Cosmos 92 Nation: USSR. Payload: Bion precursor. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 331 km (205 mi). Inclination: 64.90 deg. Period: 89.90 min. COSPAR: 1965-083A. USAF Sat Cat: 1626. Duration: 8.00 days. Decay Date: 1965-10-24. High resolution photo reconnaissance satellite; returned film capsule; also carried weather and biological experiments. References: 2, 6.
1965 October 18 - 08:30 GMT - Launch Site: Poker Flat. Launch Complex: FW. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AE07.618D. -
Auroral I / O Aeronomy mission Nation: USA. Agency: USAF. Apogee: 103 km (64 mi). References: 2.
1965 October 18 - 11:23 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL39. -
Airglow Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 205 km (127 mi). References: 2.
1965 October 19 - 05:44 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 93 Nation: USSR. Program: DS. Payload: DS-U2-V s/n 1. Mass: 305 kg (672 lb). Class: Technology. Type: Military. Spacecraft: DS-U2-V. Agency: MO SSSR. Perigee: 216 km (134 mi). Apogee: 513 km (318 mi). Inclination: 48.40 deg. Period: 91.80 min. COSPAR: 1965-084A. USAF Sat Cat: 1629. Completed Operations Date: 1965-12-16. Decay Date: 1966-01-03. Military technology development satellite - mission still classified. References: 2, 6, 99.
1965 October 19 - 17:30 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.98GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 124 km (77 mi). References: 2.
1965 October 19 - 20:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.142NA. -
Colorado / Ikeya-Seki Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 179 km (111 mi). References: 2.
1965 October 19 - 23:10 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.174GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 114 km (70 mi). References: 2.
1965 October 20 - -
NASA accepted first flight Apollo spacecraft 009 Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Apollo spacecraft 009, first of the type that would carry three astronauts to the moon and back, was accepted by NASA during informal ceremonies at North American. Spacecraft 009 included a CM, SM, launch escape system, and adapter. It went to Cape Canaveral for integration with the first Saturn IB (Saturn IB and SIVB stages received August 1965). The spacecraft was stacked on the launch vehicle on 26 December.
References: 16.
1965 October 20 - -
First coordination meeting on the S-IVB Orbital Workshop and related Apollo Applications Program activities. Nation: USA. Program: Skylab. Spacecraft: Skylab, MORL. MSC and MSFC program officials and engineers held their first coordination meeting on the S-IVB Orbital Workshop and related Apollo Applications Program experiment activities. Among the most significant results of this meeting was a request by Houston for inclusion of an artificial gravity experiment as part of the S-IVB command and service module concept of the Workshop. MSFC officials undertook to define the feasibility of such an experiment, examining several possible technical approaches (including cables a concept that MSC found less shall appealing). MSFC investigators also sought help from LaRC, where considerable work along this line had been done as part of that Center's MORL study program.
1965 October 20 - Launch Vehicle: UR-700. -
Draft project work on UR-700/LK-700 approved. Nation: USSR. Spacecraft: LK-700. Ministry of General Machine Building (MOM) Decree 'On approval of work on the draft project of the UR-700/LK-700 lunar complex' was issued. References: 474.
1965 October 20 - -
Leonov and Belyayev accused Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 2. Representatives from the Central Committee believe that, when Leonov and Belyayev discussed their spacewalk with US representatives visiting Moscow, this was used by the Americans to accelerate preparations for their own spacewalk from Gemini 4. References: 376.
1965 October 20 - Launch Site: San Nicolas. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier/551. FAILURE: Failure. -
Flight test 1 test Nation: USA. Agency: NMC. Apogee: 5.00 km (3.10 mi). References: 2.
1965 October 20 - 05:20 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL306. -
LUX Solar AC4 Solar x-ray and ultraviolet mission Nation: Australia. Agency: WRE/RAE. Apogee: 214 km (132 mi). References: 2.
1965 October 20 - 18:09 GMT - Launch Site: Vandenberg. Launch Complex: 395-C. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-33. -
Power Box Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). Operational missile test. Some lists give launch date as 10 October. References: 2.
1965 October 20 - 20:35 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.146DS. -
Comet study / Solar Ultraviolet astronomy / solar ultraviolet mission Nation: USA. Agency: NASA. Apogee: 184 km (114 mi). References: 2.
1965 October 21 - Launch Vehicle: Saturn I. Model: Saturn IB. -
Launch schedule for Apollo-Saturn IB flights revised Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Samuel C. Phillips, Apollo Program Director, notified the Center directors and Apollo program managers in Houston, Huntsville, and Cape Kennedy that OMSF's launch schedule for Apollo-Saturn IB flights had been revised, based on delivery of CSMs 009 and 011: - AS-201 - January 1966
- AS-202 - June 1966
Schedules for AS-203 through 205 (July and October 1966, and January 1967) were unchanged.
References: 16.
1965 October 21 - -
Bubble-type helmet for the Apollo extravehicular mobility unit Nation: USA. Program: Apollo. Spacecraft: A7L. MSC announced that the bubble-type helmet, designed by Crew Systems Division (CSD) engineers Robert L. Jones and James O'Kane, had been adopted for use in the Apollo extravehicular mobility unit. The new helmet was smaller and lighter than earlier types; extensive studies by CSD had demonstrated its superior comfort, visibility, and don/doff characteristics.
References: 16.
1965 October 21 - -
Planning schedule for follow-up procurement of Apollo spacecraft for the AAP. Nation: USA. Spacecraft: Apollo X. MSC Deputy Director George M. Low advised NASA Hq of Houston's planning schedule for follow-up procurement of Apollo spacecraft for the AAP. Based upon the most recent delivery schedules for the last several command and service modules and lunar excursion modules for Apollo, contract award for those vehicles was scheduled for July and August 1966. In accordance with a 14 July directive from Headquarters, MSC was preparing a procurement plan for the extended CSM and the LEM derivatives covering both the final definition and development and operational phases of AAP. Approval of this plan by Headquarters, Low stated, was anticipated for mid-December, while award of contracts for the program definition phase was set for late January 1966. The contract award date for actual development of the extended CSM was slated for October 1966, while that for the LEM derivatives was postponed until mid- 1967 (in line with revised funding directives from Washington).
1965 October 21 - 16:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.164UA. -
JHU Ikeya-Seki Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 191 km (118 mi). References: 2.
1965 October 22 - -
Gagarin writes a letter to Brezhnev Nation: USSR. Program: Lunar L1, Voskhod, Soyuz. Gagarin has sent a letter to Brezhnev, complaining of the poor organisation of the Soviet space program. The Kremlin has received it... reaction is awaited. The letter specifically cites the multitude of space projects and de-emphasis of manned efforts. Additional Details: Gagarin writes a letter to Brezhnev. References: 72, 376.
1965 October 22 - -
10 areas on the moon selected as subjects for Lunar Orbiter Nation: USA. Program: Apollo. Spacecraft: Lunar Orbiter. NASA announced that it had selected 10 areas on the moon as subjects for Lunar Orbiter's cameras during 1966. These areas encompassed most major types of lunar terrain. Most were suitable - and potential - landing sites for Surveyor and Apollo spacecraft. References: 16.
1965 October 22 - 07:54 GMT - Launch Site: Poker Flat. Launch Complex: FW. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AE07.619D. -
Auroral I / O Ionosphere mission Nation: USA. Agency: USAF. Apogee: 137 km (85 mi). References: 2.
1965 October 22 - 20:18 GMT - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. Model: Veronique AGI. LV Configuration: Veronique AGI AGI/V54. -
FU-115 Electron density Ionosphere mission Nation: France. Agency: CNES. Apogee: 210 km (130 mi). FU115 Electron density mission. References: 2.
1965 October 23 - -
Cosmonaut selection Nation: USSR. Although Kamanin desired 40 new cosmonaut-trainees, in the end only 17 were selected. They were:- Pilots: Voloshin, Sharafutdinov, Shcheglov, Kramarenko, Yakovlev, Petrushenko,Skvortsov, Fyodorov,Klimuk, Sarafanov, Zudov, Kizim
- Engineers: Kolesnikov,Stepanov Eduard, Lisun, Rozhdestvensky, Khludeyev, Glazkov, Preobrazhensky
- Navigator: Grishchenko
- Physician: Degtyarov
References: 376.
1965 October 23 - Launch Site: Hammaguira. Launch Complex: Brigitte. Launch Pad: -. Launch Vehicle: SSBS. Model: SSBS S112. LV Configuration: SSBS S112 2601. -
Essai 1 test Nation: France. Agency: DMA. Apogee: 50 km (31 mi). References: 2.
1965 October 23 - 05:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NRL ND3.167. -
Aeronomy mission Nation: USA. Agency: NRL. Apogee: 254 km (157 mi). References: 2.
1965 October 23 - 16:14 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.175GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 118 km (73 mi). References: 2.
1965 October 23 - 16:38 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.172GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 114 km (70 mi). References: 2.
1965 October 25 - -
Gemini 6 mission canceled. Nation: USA. Flight: Gemini 6. The Gemini VI mission was canceled when Gemini Agena target vehicle (GATV) 5002 suffered what appeared to be a catastrophic failure shortly after separating from the Atlas launch vehicle. The Gemini Atlas-Agena target vehicle was launched from complex 14 at 10:00 a.m., e.s.t. When the two vehicles separated at 10:05, all signals were normal. But approximately 375 seconds after liftoff, vehicle telemetry was lost and attempts to reestablish contact failed. The Gemini VI countdown was held and then canceled at 10:54 a.m., because the target vehicle had failed to achieve orbit. In accordance with Air Force Space Systems Division (SSD) procedures and NASA management instructions - both of which specified investigation in the event of such a failure - Major General Ben I. Funk, SSD Commander, reconvened the Agena Flight Safety Review Board, and NASA established a GATV Review Board.
1965 October 25 - Launch Vehicle: Proton. -
L1 manned circumlunar mission taken from Chelomei, given to Korolev. Nation: USSR. Spacecraft: Soyuz 7K-L1, Soyuz 7K-OK, LK-1. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On the Concentration of Forces of Industrial Design Organisations for the Creation of Rocket-Space Complex Means for Circling the Moon--work on the UR-500K-L1 program' was issued. As a result of a presentation to the Military Industrial Commission, Afanasyev backed Korolev in wresting control of the manned circumlunar project from Chelomei. The Chelomei LK-1 circumlunar spacecraft was cancelled. In its place, Korolev would use a derivative of the Soyuz 7K-OK, the 7K-L1, launched by Chelomei’s UR-500K, but with a Block D translunar injection stage from the N1. He envisioned launch of the unmanned 7K-L1 into low earth orbit, followed by launch and docking of a 7K-OK with the 7K-L1. The crew would then transfer to the L1, which would then be boosted toward the moon. This was the original reason for the development of the 7K-OK.
References: 474.
1965 October 25 - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. Model: Vesta. LV Configuration: Vesta 002. -
FU-123 test Nation: France. Agency: CNES. Apogee: 105 km (65 mi). References: 2.
1965 October 25 - 15:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC14. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3 Agena D. LV Configuration: SLV-3 Agena D 5301 / Agena D 5002. FAILURE: Exploded 6 minutes after takeoff. Failure. -
Gemini 6 Agena Target Nation: USA. Program: Gemini. Payload: TDA-2. Mass: 3,261 kg (7,189 lb). Class: Manned. Type: Logistics. Spacecraft: Gemini Agena Target Vehicle. Agency: NASA. COSPAR: F651025A. Decay Date: 1965-10-25. Flight: Gemini 6, Gemini 7. The Agena target vehicle failed to reach orbit. Gemini 6, awaiting launch, was cancelled. In the ashes of this setback, the idea of launching Gemini 6 to rendezvous with Gemini 7 was born. References: 126, 26, 278.
1965 October 26 - -
Thoughts on Gemini 6 Nation: USSR. Program: Gemini, Soyuz. Flight: Gemini 6. Kamanin notes the aborted first launch attempt of Gemini 6, but expects the Americans to achieve the first space docking, using the crew as pilots to fly the spacecraft. He curses Korolev and Keldysh for wasting three years trying to develop a fully automated system for Soyuz, which has put the Soviet Union well behind the Americans. He does not see any equivalent Soviet achievement until the end of 1966...
References: 376.
1965 October 26 - 12:03 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 170 km (100 mi). References: 2.
1965 October 26 - 15:25 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.53GS. -
Solar mission Nation: USA. Agency: NASA. Apogee: 195 km (121 mi). References: 2.
1965 October 27 - 18:49 GMT - Launch Site: Delamar Dry Lake DZ. Launch Complex: -. Launch Pad: 37.3 N x 114.9 W. Launch Vehicle: X-15. LV Configuration: X-15 3-51-75. -
X-15A N.Scan/BLN test Nation: USA. Agency: NASA/USAF. Apogee: 72 km (44 mi). Maximum Speed - 5662 kph. Maximum Altitude - 72210 m. References: 2.
1965 October 28 - -
The White House announced that NASA would attempt to launch Gemini VI while Gemini VII was in orbit. Nation: USA. Flight: Gemini 6, Gemini 7. The original Gemini VI mission had been canceled when its target vehicle failed catastrophically on October 25. In a memorandum to the President, NASA Administrator James E. Webb indicated the possibility that Gemini VI spacecraft and launch vehicle could be reerected shortly after the launch of Gemini VII. Since much of the prelaunch checkout of Gemini VI would not need repeating, it could be launched in time to rendezvous with Gemini VII (a mission scheduled for 14 days) if launching Gemini VII did not excessively damage the launch pad. NASA officials, spurred by suggestions from Walter F. Burke and John F. Yardley of McDonnell, began discussing the possibility of a dual mission immediately after the failure October 25, drawing on some six months of discussion and preliminary planning by NASA, Air Force, Martin, and McDonnell personnel for a rapid manned flight launch demonstration.
1965 October 28 - Launch Vehicle: Titan. Model: Titan 2. -
Gemini spacecraft No. 6 and the second stage of Gemini launch vehicle (GLV) 6 were deerected and removed from complex 19. Nation: USA. Flight: Gemini 6. GLV-6 stage I was deerected the next day. The GLV was placed in storage at the Satellite Checkout Building under guard, in an environment controlled for temperature and humidity. Bonded storage maintained the integrity of previously conducted tests to reduce testing that would have to be repeated. Spacecraft No. 6 was stored in the Pyrotechnics Installation Building at the Merritt Island Launch Area.
1965 October 28 - -
Soviet Air Force Cosmonaut Training Group 3 selected. Nation: USSR.
1965 October 28 - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sirocco. LV Configuration: Sirocco EX-1.8. -
Aeronomy mission Nation: USA. Agency: DASA. Apogee: 70 km (43 mi). References: 2.
1965 October 28 - Launch Site: White Sands. Launch Complex: LC50. Launch Pad: -. Launch Vehicle: HIBEX. -
HIBEX test Nation: USA. Agency: USA. Apogee: 0 km ( mi). References: 2.
1965 October 28 - 00:10 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.176GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 117 km (72 mi). References: 2.
1965 October 28 - 06:55 GMT - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. Model: Veronique AGI. LV Configuration: Veronique AGI AGI/V55. -
FU-115 electron density Ionosphere mission Nation: France. Agency: CNES. Apogee: 210 km (130 mi). FU115 Electron density mission. References: 2.
1965 October 28 - 08:24 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. LV Configuration: Voskhod 11A57 U15001-03. -
Cosmos 94 Nation: USSR. Payload: Bion precursor. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: MOM. Perigee: 205 km (127 mi). Apogee: 271 km (168 mi). Inclination: 65.00 deg. Period: 89.20 min. COSPAR: 1965-085A. USAF Sat Cat: 1636. Duration: 8.00 days. Decay Date: 1965-11-05. High resolution photo reconnaissance satellite; returned film capsule; also carried biological experiments. References: 2, 6.
1965 October 28 - 18:01 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 30.0 N x 120.0 W. Launch Vehicle: Iris. Model: Hydra-Iris. LV Configuration: Hydra-Iris BOX-2. -
LRL BOX-2 X-ray astronomy mission Nation: USA. Agency: USN NMC. Apogee: 194 km (120 mi). References: 2.
1965 October 28 - 21:17 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 439 / Agena D SS-01B 1620. -
KH-4A 1026 Nation: USA. Payload: KH-4A s/n 1026 / Agena D 1620. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 173 km (107 mi). Apogee: 432 km (268 mi). Inclination: 74.90 deg. Period: 90.50 min. COSPAR: 1965-086A. USAF Sat Cat: 1637. Decay Date: 1965-11-17. KH-4A. All cameras operated satisfactorily. References: 2, 6.
1965 October 29 - Launch Site: Baikonur. Launch Complex: PU33. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 October 29-30 - Launch Vehicle: Titan. Model: Titan 2. -
Gemini launch vehicle (GLV) 7 was erected at complex 19, following the deerection of GLV-6. Nation: USA. Flight: Gemini 7. Power was applied to GLV-7 on October 31, and Subsystems Reverification Tests (SSRT) began immediately. SSRT ended November 9, and the Prespacecraft Mate Verification Test was performed November 10. This test now included dropping all umbilicals, eliminating the need for a Flight Configuration Mode Test (FCMT). No FCMT was performed on GLV-7 or any subsequent vehicle.
1965 October 29 - 11:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NRL NF3.162R. -
Infrared Telescope Infrared astronomy mission Nation: USA. Agency: NRL. Apogee: 205 km (127 mi). References: 2.
1965 October - -
Seven flights were made with the Apollo Lunar Landing Research Vehicle Nation: USA. Program: Apollo. Spacecraft: Apollo LLRV. Seven flights were made with the Lunar Landing Research Vehicle at Flight Research Center during October. The first three were in support of X-15 conference activities, and the last four were for attitude control research. Five of the landings were made in the lunar simulation mode.
References: 16.
1965 November 1 - -
OKB-1 learns of Gagarin letter Nation: USSR. Program: Voskhod, Soyuz. Tsybin has learned through his Ministry of Defence contacts of Gagarin's letter to Brezhnev. He hears that they have criticized the space policy of the Minister of Defence and proposed that the VVS manage Soviet manned spaceflight. The letter also reportedly requests production of a new series of Voskhods to fill in the manned spaceflight gap created by delays in the Soyuz program. Korolev is remarkably unperturbed that he had not heard of the letter, and that Gagarin never said anything to him about it.
References: 367.
November 1965 - Launch Site: Jiuquan. Launch Complex: LA3. Launch Pad: -. Launch Vehicle: DF-2. Model: DF-2A. -
First successful test of DF-2A. Nation: China. Agency: PRC. Apogee: 200 km (120 mi). First launch of redesigned DF-2. The flight demonstrated a 20% improvement in range for the same 1500 kg payload, and replaced the radio guidance of the DF-2 with an autonoumous gyroscopic system. References: 2.
1965 November 2 - Launch Site: Baikonur. Launch Complex: PU31. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 November 2 - 12:28 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: UR-500. LV Configuration: UR-500 209. -
Proton 2 Nation: USSR. Program: Proton. Payload: N-4 s/n 2. Mass: 8,300 kg (18,200 lb). Class: Astronomy. Spacecraft: N-4 . Agency: MOM. Perigee: 189 km (117 mi). Apogee: 608 km (377 mi). Inclination: 63.50 deg. Period: 92.50 min. COSPAR: 1965-087A. USAF Sat Cat: 1701. Decay Date: 1966-02-06. High energy physics laboratory. Investigation of ultra-high-energy cosmic particles. References: 2, 6, 67, 274.
1965 November 2 - 20:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Exos. LV Configuration: Exos CRL AE13.559. -
IQSY 30-kg Sphere Aeronomy mission Nation: USA. Agency: USAF. Apogee: 686 km (426 mi). References: 2.
1965 November 2 - 23:35 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Sparrow Arcas. LV Configuration: Sparrow Arcas S-1. -
IQSY release Aeronomy / ionosphere mission Nation: USA. Agency: USAF. Apogee: 134 km (83 mi). References: 2.
1965 November 3 - Launch Vehicle: Titan. Model: Titan 2. -
Martin-Baltimore received the propellant tanks for Gemini launch vehicle (GLV) 11 from Martin-Denver, which had began fabricating them June 28. Nation: USA. Flight: Gemini 10, Gemini 11. They were shipped by rail October 27. The GLV-11 stage II fuel tank was used in GLV-10, and the stage II fuel tank from GLV-12 was reassigned to GLV-11, arriving by air from Martin-Denver January 16, 1966. Aerojet-General delivered the engines for GLV-11 on December 14, 1965. Stage I tank splicing and engine installation was complete by March 31, stage II by April 5. Stage I horizontal tests ended April 12 and stage II, April 25.
1965 November 3 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. FAILURE: Failure. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1965 November 3 - 09:17 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun CRL AE6.557. -
IQSY 7-inch Sphere Aeronomy mission Nation: USA. Agency: USAF. Apogee: 137 km (85 mi). References: 2.
1965 November 3 - 17:09 GMT - Launch Site: Cuddeback Dry Lake DZ. Launch Complex: -. Launch Pad: 35.3 N x 117.5 W. Launch Vehicle: X-15. LV Configuration: X-15 2-43-75. -
X-15A-2 External Tank test Nation: USA. Agency: NASA/USAF. Apogee: 21 km (13 mi). First flight with empty external tanks. Ammonia tank recovered; Lox tank destroyed. Maximum Speed - 2414 kph. Maximum Altitude - 21520 m. References: 2.
1965 November 3 - 19:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 CRL AE3.520. -
Solar XUVT Solar soft x-ray mission Nation: USA. Agency: USAF. Apogee: 210 km (130 mi). References: 2.
1965 November 4 - Launch Site: Baikonur. Launch Complex: LC41/3. Launch Pad: LC41/3?. Launch Vehicle: R-16. Model: R-16U. -
Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1965 November 4 - 05:31 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 95 Nation: USSR. Program: DS. Payload: DS-U2-V s/n 2. Mass: 325 kg (716 lb). Class: Technology. Type: Military. Spacecraft: DS-U2-V. Agency: MO SSSR. Perigee: 211 km (131 mi). Apogee: 521 km (323 mi). Inclination: 48.40 deg. Period: 91.90 min. COSPAR: 1965-088A. USAF Sat Cat: 1706. Completed Operations Date: 1965-11-04. Decay Date: 1966-01-18. Military technology development satellite - mission still classified. References: 2, 6, 99.
1965 November 4 - 17:11 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 1-62-103. FAILURE: Two engine relights required. -
X-15A Checkout mission Nation: USA. Agency: NASA/USAF. Apogee: 24 km (14 mi). Maximum Speed - 4450 kph. Maximum Altitude - 24440 m. References: 2.
1965 November 5 - -
International Latex to build Apollo space suit, and Hamilton Standard portable life support system Nation: USA. Program: Apollo. Spacecraft: A7L. NASA announced that it would negotiate with International Latex Corporation for an estimated $10 million contract to fabricate the Apollo space suit consisting of the liquid-cooled undergarment, constant wear garment, pressure garment assembly, and thermo-micrometeoroid protective overgarment. At the same time an estimated $20 million contract was negotiated with Hamilton Standard Division of United Aircraft Corporation for continued development and manufacture of the portable life support system with a four-hour main power supply subjected to a maximum stowage soak temperature of 328K (130 degrees F).
References: 16.
1965 November 5 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1965 November 5 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1965 November 5 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1965 November 5 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1965 November 5 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. FAILURE: Failure. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1965 November 5 - Launch Site: Green River. Launch Complex: Pad 1. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena D007. -
USAF D007 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1965 November 6 - 18:38 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta E. LV Configuration: Thor Delta E 457/D34. -
Explorer 29 Nation: USA. Program: Explorer. Payload: GEOS A. Mass: 175 kg (385 lb). Class: Solar. Spacecraft: GEOS. Agency: NASA GSF. Perigee: 1,120 km (690 mi). Apogee: 2,269 km (1,409 mi). Inclination: 59.40 deg. Period: 120.30 min. COSPAR: 1965-089A. USAF Sat Cat: 1726. The primary objective of GEOS-A was to provide global geodetic measurements for determining the positions of fiducial control points on the Earth to an accuracy of 10 meters in an Earth centre of mass co-ordinate system, and to determine the structure of the Earth's gravity field to 5 parts in 10 million. Instrumentation included (1) four optical beacons, (2) laser reflectors, (3) a radio range transponder, (4) Doppler beacons, and (5) a range and range rate transponder. These were designed to operate simultaneously to fulfil the objectives of locating observation points (geodetic control stations) in a three dimensional earth centre-of-mass co-ordinate system within 10 m of accuracy, of defining the structure of the earth's irregular gravitational field and refining the locations and magnitudes of the large gravity anomalies, and of comparing results of the various systems onboard the spacecraft to determine the most accurate and reliable system. In January 1967, a failure in the satellite's command system rendered several geodetic systems inoperable. Radio doppler measurements and the passive laser reflector experiment could continue indefinitely, however.
Additional Details: Explorer 29. References: 2, 6, 405.
1965 November 8 - Launch Vehicle: Titan. Model: Titan 2. -
The Combined Systems Acceptance Test of Gemini launch vehicle (GLV) 8 was conducted at Martin-Baltimore. Nation: USA. Flight: Gemini 8. The vehicle acceptance team convened November 16 and completed its inspection November 19, deeming the vehicle excellent. GLV-8 was deerected December 13-14 and was formally accepted by the Air Force on December 23. Stage I was airlifted to Cape Kennedy on January 4, 1966, followed by stage II on January 6. Both stages were placed in storage.
1965 November 8 - 05:05 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 10. LV Configuration: Kappa 10 K-10-1. -
Test / ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 228 km (141 mi). References: 2.
1965 November 8 - 19:26 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3 Agena D. LV Configuration: SLV-3 Agena D 7113 / Agena D 7113. -
KH 7-23 Nation: USA. Payload: KH-7 no. 23. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-7. Agency: NRO/USAF. Perigee: 280 km (170 mi). Apogee: 352 km (218 mi). Inclination: 93.90 deg. Period: 90.80 min. COSPAR: 1965-090A. USAF Sat Cat: 1727. Decay Date: 1965-11-11. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
-
OPS 6232/Agena D Nation: USA. Payload: Agena Pickaback. Mass: 60 kg (132 lb). Class: Sigint. Spacecraft: SSF. Agency: USAF. Perigee: 155 km (96 mi). Apogee: 284 km (176 mi). Inclination: 93.90 deg. Period: 88.90 min. COSPAR: 1965-090B. USAF Sat Cat: 1728. Decay Date: 1965-11-09. Not identified as a subsatellite ferret by McDowell. References: 2, 6, 172, 278.
1965 November 9 - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ Nike Hydac. -
Aeronomy mission? [113 kg] Nation: USA. Agency: USAF. Apogee: 521 km (323 mi). References: 2.
1965 November 9 - Launch Site: Vandenberg. Launch Complex: LF21. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2009. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1965 November 9 - 09:58 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 179. -
Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi). References: 2.
1965 November 9 - 18:40 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.168UA. -
UM Pitot 18 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 144 km (89 mi). References: 2.
1965 November 9 - 19:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 CRL AF3.523. -
Extreme ultraviolet Mon Solar extreme ultraviolet mission Nation: USA. Agency: USAF. Apogee: 238 km (147 mi). References: 2.
1965 November 9 - 19:16 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.03GA. -
Thermosphere Aeronomy mission Nation: USA. Agency: NASA. Apogee: 328 km (203 mi). References: 2.
1965 November 10 - 02:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 CRL AD3.356. -
Lunar Infrared Infrared astronomy mission Nation: USA. Agency: USAF. Apogee: 180 km (110 mi). References: 2.
1965 November 10 - 07:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.02GA. -
Thermosphere Aeronomy mission Nation: USA. Agency: NASA. Apogee: 328 km (203 mi). References: 2.
1965 November 11 - -
Apollo Block I SPS engine altitude qualification test Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The Block I service propulsion system engine successfully completed the first altitude qualification tests at AEDC. References: 16.
1965 November 11 - 04:10 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun CRL AE6.378. -
DAPHNE Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 113 km (70 mi). References: 2.
1965 November 11 - 04:15 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Sparrow Arcas. LV Configuration: Sparrow Arcas S-2. -
Aeronomy / ionosphere mission Nation: USA. Agency: USAF. Apogee: 137 km (85 mi). References: 2.
1965 November 12 - -
Apollo portable life support system Preliminary Design Review Nation: USA. Program: Apollo. Spacecraft: A7L. The portable life support system Preliminary Design Review was completed. The design was essentially complete and no major discrepancies were noted during the review. References: 16.
1965 November 12 - -
USAF MOL Astronaut Training Group 1 selected. Nation: USA. The group was selected to provide crews for flights of the Manned Orbiting Laboratory, a classified military manned space station.. Qualifications: Qualified military pilot; graduate of Aerospace Research Pilot School; serving military officer; US citizen by birth..
1965 November 12 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Military training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1965 November 12 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-84. -
Environment Aeronomy mission Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi). References: 2.
1965 November 12 - 05:02 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. -
Venera 2 Nation: USSR. Program: Venera. Payload: 3MV-4 s/n 4. Mass: 962 kg (2,120 lb). Class: Planetary. Type: Venus. Spacecraft: Venera 3MV-4. Agency: MOM. Perigee: 205 km (127 mi). Apogee: 315 km (195 mi). Inclination: 51.80 deg. Period: 89.71 min. COSPAR: 1965-091A. USAF Sat Cat: 1730. Venera 2 was launched towards the planet Venus and carried a TV system and scientific instruments. On February 27, 1966, the spacecraft passed Venus at a distance of 24,000 km and entered a heliocentric orbit. The spacecraft system had ceased to operate before the planet was reached and returned no data.
References: 2, 6, 64, 296.
1965 November 12 - 22:28 GMT - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1 C2X-4. -
STAFF 4 test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1965 November 13 - Launch Vehicle: Proton. -
Industrial orders to cancel LK-1 spacecraft and implement L1. Nation: USSR. Spacecraft: Soyuz 7K-L1, LK-1. Ministry of General Machine Building (MOM) Decree 'On work on the UR-500K-L1 program' was issued. References: 474.
1965 November 14 - Launch Site: Baikonur. Launch Complex: PU32. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 November 16 - 02:09 GMT - Launch Site: Niijima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: ST. LV Configuration: ST ST-I F1. -
Test mission Nation: Japan. Agency: STA. Apogee: 20 km (12 mi). References: 2.
1965 November 16 - 04:19 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. -
Venera 3 Nation: USSR. Program: Venera. Payload: 3MV-3 s/n 1. Mass: 958 kg (2,112 lb). Class: Planetary. Type: Venus. Spacecraft: Venera 3MV-3. Agency: MOM. COSPAR: 1965-092A. USAF Sat Cat: 1733. Decay Date: 1966-03-01. Venera 3 was launched towards the planet Venus. The mission was to land on the Venusian surface. The entry vehicle contained a radio communication system, scientific instruments, electrical power sources, and medallions bearing the coat of arms of the U.S.S.R. The station impacted Venus on March 1, 1966. However, the communications systems had failed before planetary data could be returned.
References: 2, 6, 64, 296.
1965 November 16 - 16:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.119NA. -
LUSTER B Meteorites mission Nation: USA. Agency: NASA. Apogee: 144 km (89 mi). References: 2.
1965 November 16 - 18:22 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun CRL AE6.379. -
D-region comparison Ionosphere / aeronomy mission Nation: USA. Agency: USAF. Apogee: 114 km (70 mi). References: 2.
1965 November 16 - 22:15 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. -
YORKSHIRE Aeronomy mission Nation: USA. Agency: USAF. Apogee: 130 km (80 mi). References: 2.
1965 November 16 - 23:00 GMT - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ Nike Nike. LV Configuration: HJ Nike Nike Sandia 152-90. -
LRL RCS-1 Aeronomy mission Nation: USA. Agency: Sandia. Apogee: 183 km (113 mi). References: 2.
1965 November 17 - 04:25 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.238UE. -
Auroral emissions Aurora mission Nation: USA. Agency: NASA. Apogee: 178 km (110 mi). References: 2.
1965 November 17 - 06:34 GMT - Launch Site: Niijima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: NAL-16. LV Configuration: NAL-16 NAL-16TR. -
Test mission Nation: Japan. Agency: STA. Apogee: 45 km (27 mi). References: 2.
1965 November 17 - 23:36 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun CRL AE6.484. -
EDNA Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 155 km (96 mi). References: 2.
1965 November 18 - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. Model: Nike Javelin. -
IQSY Na, TMA Aeronomy sodium / TMA release mission Nation: USA. Agency: AFCRL. Apogee: 130 km (80 mi). References: 2.
1965 November 18 - 02:20 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Sparrow Arcas. LV Configuration: Sparrow Arcas NA-FLORA /S-4. -
Aeronomy mission Nation: USA. Agency: USAF. Apogee: 130 km (80 mi). References: 2.
1965 November 18 - 05:20 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Sparrow Arcas. LV Configuration: Sparrow Arcas S-3. -
Aeronomy mission Nation: USA. Agency: USAF. Apogee: 130 km (80 mi). References: 2.
1965 November 18 - 05:20 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun CRL AE6.382. -
IQSY D-region comparison Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 116 km (72 mi). References: 2.
1965 November 18 - 08:01 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Sparrow Arcas. LV Configuration: Sparrow Arcas NA-HANNAH /S-6. -
Aeronomy / ionosphere mission Nation: USA. Agency: USAF. Apogee: 137 km (85 mi). References: 2.
1965 November 18 - 11:21 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun CRL AE6.499. -
POLLY Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 155 km (96 mi). References: 2.
1965 November 18 - 14:31 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.78UA. -
Pandora 1 (Leonids) Meteorites mission Nation: USA. Agency: NASA. Apogee: 149 km (92 mi). References: 2.
1965 November 18 - 17:45 GMT - Launch Site: Hammaguira. Launch Complex: Bechar. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C119. -
MPE Ba-14 Aeronomy mission Nation: France. Agency: CNES. Apogee: 170 km (100 mi). References: 2.
1965 November 19 - Launch Vehicle: Titan. Model: Titan 2. -
Aerojet-General delivered the stage II engine for Gemini launch vehicle (GLV) 10 to Martin-Baltimore. Nation: USA. Flight: Gemini 10, Gemini 11. The stage I engine had been delivered August 23. Martin-Baltimore completed splicing stage I January 12, 1966; stage II splicing, using the fuel tank reassigned from GLV-11, was finished February 2. Engine installation was completed February 7, and stage I horizontal tests February 11. Stage II horizontal testing ended March 2.
1965 November 19 - 04:48 GMT - Launch Site: Wallops Island. Launch Complex: LA3A. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-4. LV Configuration: Scout X-4 S138R. -
Explorer 30 Nation: USA. Program: Explorer. Payload: Solar Explorer A. Mass: 57 kg (125 lb). Class: Solar. Spacecraft: IQSY. Agency: NRL. Perigee: 671 km (416 mi). Apogee: 856 km (531 mi). Inclination: 59.70 deg. Period: 100.10 min. COSPAR: 1965-093A. USAF Sat Cat: 1738. Solar radiation data. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1965 November 19 - 04:54 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL130. -
Solar X-rays / SpE / Li Ionosphere / solar x-rays mission Nation: Australia. Agency: WRE/RAE. Apogee: 138 km (85 mi). References: 2.
1965 November 19 - 17:45 GMT - Launch Site: Hammaguira. Launch Complex: Bechar. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C120. -
MPE Ba-15 Aeronomy mission Nation: France. Agency: CNES. Apogee: 190 km (110 mi). References: 2.
1965 November 20 - 00:37 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache Ferdinand 12. -
Ferdinand 12 Ionosphere mission Nation: Norway. Agency: NDRE. Apogee: 122 km (75 mi). References: 2.
1965 November 20 - 05:20 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.239UE. -
Auroral emissions Aurora mission Nation: USA. Agency: NASA. Apogee: 175 km (108 mi). References: 2.
1965 November 20 - 08:28 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 KP3.8. -
Stellar Spectra Ultraviolet astronomy mission Nation: USA. Agency: KPNO. Apogee: 150 km (90 mi). References: 2.
1965 November 20 - 17:53 GMT - Launch Site: Hammaguira. Launch Complex: Bechar. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 1. LV Configuration: Dragon D-8. -
MPE Ba-16? Aeronomy mission Nation: France. Agency: CNES. Apogee: 404 km (251 mi). References: 2.
1965 November 22 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-12 Sandia 152-89. FAILURE: Failure. -
HRT Aeronomy mission Nation: USA. Agency: Sandia. Apogee: 270 km (160 mi). References: 2.
1965 November 22 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-27. -
Sampler Aeronomy mission Nation: USA. Agency: Sandia. Apogee: 200 km (120 mi). References: 2.
1965 November 22 - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena B007. FAILURE: Failure. -
USN B007 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 0 km ( mi). References: 2.
1965 November 22 - 06:35 GMT - Launch Site: Niijima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Lambda. Model: LS-A. LV Configuration: LS-A-3. -
Test mission Nation: Japan. Agency: STA. Apogee: 150 km (90 mi). References: 2.
1965 November 23 - -
Fire during Apollo CM RCS test for spacecraft 009 Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. North American informed MSC of a fire in the reaction control system (RCS) test cell during a CM RCS test for spacecraft 009. The fire was suspected to have been caused by overheating the test cell when the 10 engines were activated, approximately 30 sec prior to test completion. An estimated test delay of two to three weeks, due to shutdown of the test cell for refurbishment, was forecast. MSC informed the Apollo Program Director that an investigation was underway.
References: 16.
1965 November 23 - Launch Vehicle: Spiral 50-50. -
Spiral spaceplane Nation: USSR. Spacecraft: Spiral OS. Gagarin, Belyayev, and Leonov are preparing for a meeting with Brezhnev. Nothing controversial is to be raised. The real issue now is to develop a winged, manned orbital spacecraft, and a winged booster stage for space launches. This will be essential to future manned military activities. Mikoyan's MiG bureau has been working on the orbital spaceplane, and Tupolev the winged booster stage. Titov, Filipchenko, and Matinchenko and a few other cosmonauts will coordinate with Mikoyan on development of the spaceplane design.
References: 376.
1965 November 23 - 03:21 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. FAILURE: At T+528 sec, during the final thrust phase of the Block I's 8D715K engine, one of the combustion chambers blew up due to a tear in the fuel pipeline. This resulted in an abnormal separation of the upper stages. -
Cosmos 96 Nation: USSR. Program: Venera. Payload: 3MV-4 s/n 6. Mass: 960 kg (2,110 lb). Class: Planetary. Type: Venus. Spacecraft: Venera 3MV-4. Agency: MOM. Perigee: 222 km (137 mi). Apogee: 296 km (183 mi). Inclination: 51.90 deg. Period: 89.70 min. COSPAR: 1965-094A. USAF Sat Cat: 1742. Decay Date: 1965-12-09. The escape stage Block L entered parking orbit tumbling and was not able to operate properly. References: 2, 6, 64, 65.
1965 November 24 - -
Kamanin and Korolev Nation: USSR. Program: Voskhod, Soyuz, Lunar L1. Spacecraft: Voskhod, Soyuz 7K-OK, Soyuz 7K-L1. Flight: Voskhod 3, Voskhod 4, Voskhod 5, Voskhod 6, Voskhod 7, Soyuz 1, Soyuz 2A, Soyuz 3A, Soyuz 4A. Kamanin has his first face-to-face meeting with Korolev in 3 months - the longest delay in three years of working together. Their relationship is at low ebb. Despite having last talked about the next Voskhod flight by the end of November, Korolev now reveals that the spacecraft are still incomplete, and that he has abandoned plans to finish the last two (s/n 8 and 9), since these would overlap with planned Soyuz flights. By the first quarter of 1966 OKB-1 expects to be completing two Soyuz spacecraft per quarter, and by the end of 1966, one per month. Voskhod s/n 5, 6, and 7 will only be completed in January-February 1966. Korolev has decided to delete the artificial gravity experiment from s/n 6 and instead fly this spacecraft with two crew for a 20-day mission. The artificial gravity experiment will be moved to s/n 7. Completion of any of the Voskhods for spacewalks has been given up; future EVA experiments will be conducted from Soyuz spacecraft. Korolev says he has supported VVS leadership of manned spaceflight in conversations with Tyulin, Afanasyev, Pashkov, and Smirnov.
References: 376.
1965 November 24 - 04:04 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.124UE. -
Auroral emissions Aurora mission Nation: USA. Agency: NASA. Apogee: 175 km (108 mi). References: 2.
1965 November 24 - 15:37 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.242UE. -
B Field Plasma mission Nation: USA. Agency: NASA. Apogee: 169 km (105 mi). References: 2.
1965 November 25 - 04:40 GMT - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C91. -
Aeronomy mission Nation: Argentina. Agency: Argentina. Apogee: 175 km (108 mi). References: 2.
1965 November 25 - 08:24 GMT - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C93. -
Aeronomy mission Nation: Argentina. Agency: Argentina. Apogee: 175 km (108 mi). References: 2.
1965 November 25 - 13:20 GMT - Launch Site: Woomera. Launch Complex: LA5B. Launch Pad: LA5B?. Launch Vehicle: Black Knight. Model: Black Knight 301/C2. LV Configuration: Black Knight-301/C2 BK.25. -
Dazzle re-entry vehicle test Nation: UK. Agency: RAE. Apogee: 632 km (392 mi). References: 2.
1965 November 26 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M. -
Venus launch delayed. Nation: USSR. Program: Venera. Payload: 3MV-3. Class: Planetary. Type: Venus. Spacecraft: Venera 3MV-3. Decay Date: 1965-11-26. The launch attempt was abandoned due to a launch vehicle malfunction during pre-launch preparations. References: 64.
1965 November 26 - 08:24 GMT - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C96. -
Aeronomy mission Nation: Argentina. Agency: Argentina. Apogee: 175 km (108 mi). References: 2.
1965 November 26 - 12:14 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 97 Nation: USSR. Program: DS. Payload: DS-U2-M s/n 1. Mass: 267 kg (588 lb). Class: Technology. Spacecraft: DS-U2-M. Agency: MO SSSR. Perigee: 214 km (132 mi). Apogee: 2,144 km (1,332 mi). Inclination: 48.40 deg. Period: 108.90 min. COSPAR: 1965-095A. USAF Sat Cat: 1777. Completed Operations Date: 1966-01-23. Decay Date: 1967-04-02. Development tests of atomic clocks. References: 2, 6, 99.
1965 November 26 - 14:47 GMT - Launch Site: Hammaguira. Launch Complex: Brigitte. Launch Pad: -. Launch Vehicle: Diamant. Model: Diamant A. LV Configuration: Diamant A No. 1. -
Asterix 1 Nation: France. Payload: A 1. Mass: 42 kg (92 lb). Class: Technology. Spacecraft: Asterix. Agency: CNES. Perigee: 527 km (327 mi). Apogee: 1,697 km (1,054 mi). Inclination: 34.30 deg. Period: 107.50 min. COSPAR: 1965-096A. USAF Sat Cat: 1778. First French satellite. French scientific satellite 'A-I'. Launched from Hammaguir (Algeria) in rder to test the 'Diamant' launching vehicle for the first time. References: 2, 6.
1965 November 27 - Launch Site: Baikonur. Launch Complex: PU33. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 November 27 - 08:24 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. LV Configuration: Vostok 8A92 U15001-05. -
Cosmos 98 Nation: USSR. Payload: Zenit-2 11F61 s/n 31. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: MOM. Perigee: 205 km (127 mi). Apogee: 547 km (339 mi). Inclination: 65.00 deg. Period: 92.10 min. COSPAR: 1965-097A. USAF Sat Cat: 1780. Duration: 8.00 days. Decay Date: 1965-12-05. Area survey photo reconnaissance satellite. References: 2, 6,93.
1965 November 27 - 10:00 GMT - Launch Site: Vandenberg. Launch Complex: 395-D. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-20. -
Red Wagon operational test Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1965 November 28 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. -
Last Thor/Agena launch from Vandenberg AFB Nation: USA. Last Thor/Agena launch from Vandenberg AFB (first mission on 28 February 1959). References: 88.
1965 November 29 - Launch Site: San Nicolas. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. -
Project Defender Redstone launch. Nation: USA. Redstone launched as ballistic missile target and was successfully intercepted by a US Navy Terrier surface-to-air missile launched from Point Mugu, California.
1965 November 29 - 04:48 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2 Agena B. LV Configuration: Thor SLV-2 Agena B 453 (TA5) / Agena B S-01 6102. -
Alouette 2 Nation: Canada. Payload: Alouette 2 / Explorer 31. Mass: 145 kg (319 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Alouette. Agency: DRTE. Perigee: 503 km (312 mi). Apogee: 2,666 km (1,656 mi). Inclination: 79.80 deg. Period: 117.90 min. COSPAR: 1965-098A. USAF Sat Cat: 1804. Ionospheric research; data correlated with Explorer 31. The double-launch project, known as ISIS-X was the first in a new co-operative NASA-Canadian Defense Research Board program for International Satellites for Ionospheric Studies. Alouette was in orbit with an apogee just over a kilometre lower than Explorer 31's and with a perigee of just more than a kilometre higher. The orbits were some 3000 km at apogee and 500 km at perigee.
References: 2, 6.
-
Explorer 31 Nation: USA. Program: Explorer. Payload: DME A. Mass: 99 kg (218 lb). Class: Earth. Type: Ionosphere. Spacecraft: DME. Agency: NASA GSF. Perigee: 505 km (313 mi). Apogee: 2,833 km (1,760 mi). Inclination: 79.80 deg. Period: 119.70 min. COSPAR: 1965-098B. USAF Sat Cat: 1806. Ionospheric research; data correlated with Alouette 2. The Explorer 31, Direct Measurement Explorer, was launched with a Canadian Alouette II on November 28, 1965, on a Thor-Agena rocket from Vandenberg Air Force Base, California. The double-launch project, known as ISIS-X was the first in a new co-operative NASA-Canadian Defense Research Board program for International Satellites for Ionospheric Studies. Explorer 31 was in orbit with an apogee just over a kilometre more than Alouette's and with a perigee of just more than a kilometre lower. The orbits were some 3000 km at apogee and 500 km at perigee. Eight ionospheric measurement experiments sampled the environment both forward and after the satellite's path.
References: 2, 6.
1965 November 29 - 14:30 GMT - Launch Site: Vandenberg. Launch Complex: 576A1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 200D. -
NTMP KX-33 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi). References: 2.
1965 November 30 - -
Apollo Mission Simulator No 1 shipped Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Apollo Mission Simulator No. 1 was shipped from Link Group, General Precision, Binghamton, New York, to MSC. References: 16.
1965 November 30 - -
Problems with the Igla system for Soyuz Nation: USSR. Program: Voskhod, Soyuz. Spacecraft: Voskhod, Soyuz 7K-OK. Flight: Voskhod 3, Voskhod 4, Voskhod 5, Voskhod 6, Voskhod 7, Soyuz 1, Soyuz 2A, . After a meeting with Kamanin, Korolev tells Chertok in confidence that Gagarin is training for a flight on a Soyuz mission. Chertok responds that it will take him at least a year to complete training, but that doesn't matter, since Mnatsakanian's Igla docking system will not be ready than any earlier than that. Korolev explodes on hearing this. "I allowed all work on Voskhod stopped so that the staff can be completely dedicated to Soyuz. I will not allow the Soyuz schedule to slip a day further". Turkov had been completing further Voskhods only on direct orders from the VPK and on the insistence of the VVS. Aside from military experiments, further Voskhod flights were meant to take back the space endurance record from the Americans. Korolev has derailed those plans without openly telling anyone in order to get the Soyuz flying.
References: 367.
1965 November 30 - Launch Site: San Nicolas. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. -
DAT-371 Target mission Nation: USA. Agency: USA/ARPA. Apogee: 50 km (31 mi). Redstone launched as ballistic missile target for a US Navy Terrier surface-to-air missile launched from Point Mugu, California. It was reported that there were two Redstone launches as part of Project Defender from November 30 to December 13, 1965, but details of the second launch are not known.
References: 2.
1965 November 30 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. FAILURE: Failure. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1965 November - -
Ten flights were made with the Apollo lunar landing research vehicle Nation: USA. Program: Apollo. Spacecraft: Apollo LLRV. Ten flights were made with the lunar landing research vehicle. All flights were for attitude control and handling qualities research. Landings on all flights were made in the lunar landing mode. References: 16.
1965 November 30 - 07:48 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.155GG. -
Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 179 km (111 mi). References: 2.
1965 November 30 - 14:44 GMT - Launch Site: Vandenberg. Launch Complex: 395-B. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-4. -
Cross Fire operational test Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1965 December 1 - -
Green light to begin the Saturn IVB Orbital Workshop program Nation: USA. Spacecraft: Orbital Workshop. George E. Mueller, Associate Administrator for Manned Space Flight, and MSFC Director Wernher von Braun discussed Marshall's briefing on the S-IVB Workshop concept presented at Headquarters the previous day. Mueller asked that MSFC formulate a program development plan and present it at the next meeting of the Manned Space Flight Management Council. Specifically, Mueller demanded that the plan include experiments to be carried aboard the Workshop; funding arrangements; and where development work should be done (in house, or elsewhere). In addition, he asked that MSFC submit two such plans, one for the unpressurized and another for the pressurized version of the Workshop. In effect, Mueller gave Marshall the 'green light' to begin the Orbital Workshop program. At von Braun's request, the Workshop received the status of a separate project, with William Ferguson as Project Manager.
1965 December 1 - Launch Site: Sary Shagan. Launch Complex: LC6. Launch Pad: -. Launch Vehicle: A-35. Model: A-350Zh. LV Configuration: A-350Zh 6TYa?. -
Test mission Nation: USSR. Agency: PRO. Apogee: 100 km (60 mi). References: 2.
1965 December 1 - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Verification Operational test Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1965 December 1 - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Verification Operational test Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1965 December - -
Boeing report for the proposed multipurpose mission module. Nation: USA. Spacecraft: LORL. The Boeing Company submitted a utilization study report to MSC for the proposed multipurpose mission module. The report was one of 13 volumes prepared by Boeing's Aerospace Group Space Division under an MSC contract. Additional Details: Boeing report for the proposed multipurpose mission module..
1965 December - -
Experiment proposals for the immediate post-Apollo Earth-orbital phase of manned space exploration, as part of the AES program. Nation: USA. Spacecraft: Apollo X. The Advanced Missions Division, Manned Space Science Program, in the Office of Space Sciences and Applications, released details of experiment proposals submitted by teams of potential experimenters for the immediate post-Apollo Earth-orbital phase of manned space exploration, as part of the AES program. As well as detailed descriptions of the various scientific experiments themselves, the report examined the justification for AES in relation to other space programs, mission objectives, operational constraints, and long-range plans and goals.
1965 December - Launch Vehicle: RT-1. -
Work ended on the experimental RT-1 missile. Nation: USSR. The tests on this missile proved concepts and hardware for the RT-2 operational solid propellant ICBM
1965 December 2 - -
Apollo LEM TM-5 cancelled Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Maj. Gen. Samuel C. Phillips, NASA Apollo Program Director, approved the deletion of the LEM TM-5 from the ground test program. Additional Details: Apollo LEM TM-5 cancelled. References: 16.
1965 December 2 - 17:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.145GS. -
Mg II heliogram 2 Solar ultraviolet mission Nation: USA. Agency: NASA. Apogee: 185 km (114 mi). References: 2.
1965 December 3 - 10:46 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 U103-28. -
Luna 8 Nation: USSR. Program: Luna. Payload: E-6 s/n 12. Mass: 1,550 kg (3,410 lb). Class: Planetary. Type: Lunar. Spacecraft: Luna E-6. Agency: MOM. COSPAR: 1965-099A. USAF Sat Cat: 1810. Decay Date: 1965-12-06. Lunar soft landing attempt failed. Luna 8's objectives were to test a soft lunar landing system and scientific research. Weighing 1,552 kg (3,422 lbs), the spacecraft was following a trajectory close to the calculated one and the equipment was functioning normally. However, the retrofire was late, and the spacecraft impacted the lunar surface in the Sea of Storms. Tass reported that "the systems were functioning normally at all stages of the landing except the final touchdown." The mission did complete the experimental development of the star-orientation system and ground control of radio equipment, flight trajectory, and other instrumentation.
References: 2, 6, 16, 64, 296.
1965 December 4 - Launch Vehicle: Titan. Model: Titan 2. -
Both stages of Gemini launch vehicle (GLV) 6 were removed from storage and arrived at complex 19 two hours after the launch of Gemini VII. Nation: USA. Spacecraft: G5C. Flight: Gemini 6, Gemini 7. Spacecraft No. 6 was returned to complex 19 on December 5. Within 24 hours after the launch of Gemini VII, both stages of GLV-6 were erected, spacecraft and launch vehicle were mated, and power was applied. Subsystems Reverification Tests were completed December 8. The only major problem was a malfunction of the spacecraft computer memory. The computer was replaced and checked out December 7-8. The Simulated Flight Test, December 8-9, completed prelaunch tests. The launch, initially scheduled for December 13, was rescheduled for December 12.
1965 December 4 - 19:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC19. Launch Pad: -. Launch Vehicle: Titan. Model: Titan II GLV. LV Configuration: Titan II GLV GT-7 / 62-12562. -
Gemini 7 Nation: USA. Program: Gemini. Payload: Gemini SC7. Mass: 3,663 kg (8,075 lb). Class: Manned. Type: Spacecraft. Spacecraft: Gemini. Location of Spacecraft: National Air and Space Museum (Smithsonian Institution), Washington, DC. Agency: NASA MSC. Perigee: 217 km (134 mi). Apogee: 318 km (197 mi). Inclination: 28.90 deg. Period: 89.90 min. COSPAR: 1965-100A. USAF Sat Cat: 1812. Duration: 13.77 days. Decay Date: 1965-12-18. Crew: Borman, Lovell. Flight: Gemini 6, Gemini 7. Primary objectives of the mission were demonstrating manned orbital flight for approximately 14 days and evaluating the physiological effects of a long-duration flight on the crew. Among the secondary objectives were providing a rendezvous target for the Gemini VI-A spacecraft, stationkeeping with the second stage of the launch vehicle and with spacecraft No. 6, conducting 20 experiments, using lightweight pressure suits, and evaluating the spacecraft reentry guidance capability. All objectives were successfully achieved with the exception of two experiments lost because of equipment failure. Shortly after separation from the launch vehicle, the crew maneuvered the spacecraft to within 60 feet of the second stage and stationkept for about 15 minutes. The exercise was terminated by a separation maneuver, and the spacecraft was powered down in preparation for the 14-day mission. The crew performed five maneuvers during the course of the mission to increase orbital lifetime and place the spacecraft in proper orbit for rendezvous with spacecraft No. 6. Rendezvous was successfully accomplished during the 11th day in orbit, with spacecraft No. 7 serving as a passive target for spacecraft No. 6. About 45 hours into the mission, Lovell removed his pressure suit. He again donned his suit at 148 hours, while Borman removed his. Some 20 hours later Lovell again removed his suit, and both crewmen flew the remainder of the mission without suits, except for the rendezvous and reentry phases. With three exceptions, the spacecraft and its systems performed nominally throughout the entire mission. The delayed-time telemetry playback tape recorder malfunctioned about 201hours after liftoff, resulting in the loss of all delayed-time telemetry data for the remainder of the mission. Two fuel cell stacks showed excessive degradation late in the flight and were taken off the line; the remaining four stacks furnished adequate electrical power until reentry. Two attitude thrusters performed poorly after 283 hours in the mission. Retrofire occurred exactly on time, and reentry and landing were nominal. The spacecraft missed the planned landing point by only 10.3 km miles, touching down on December 18. The crew arrived at the prime recovery ship, the aircraft carrier Wasp, half an hour later. The spacecraft was recovered half an hour after the crew. Far surpassing the Gemini 5 flight, Gemini 7 set a manned spaceflight endurance record that would endure for years. The incredibly boring mission, was made more uncomfortable by the extensive biosensors. This was somewhat offset by the soft spacesuits (used only once) and permission to spend most of the time in long johns. The monotony was broken just near the end by the rendezvous with Gemini 6.
References: 2, 6, 16, 26, 33,60.
1965 December 6 - -
Space race Nation: USSR. Flight: Gemini 7. Kamanin notes the Luna 8 mission, which will attempt the first soft landing on the moon the next day, and the launch of Gemini 7, which is to set a new space endurance record and make the first rendezvous in space. The Americans are clearly pulling well ahead of the Soviet Union, but Kamanin vows not to capitulate. He recaps the opposition of Malinovskiy, Smirnov, and Ustinov to manned spaceflight over the last five years. Korolev and Kamanin already wanted to build a second series of ten Vostok spacecraft in 1961, which could have been used to keep the lead in the race with America. Instead this was blocked year after year. The cosmonauts have been trained and ready for the fights aboard Vostok or Voskhod that would have kept the Soviet Union ahead in the space race; what has been lacking is the spacecraft to make the flights.
References: 376.
1965 December 6 - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena C017. -
USAF C017 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1965 December 6-17 -
1965 December 6 - 10:24 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 151. -
Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi). References: 2.
1965 December 6 - 19:26 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-42. -
OT/GT7 target Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1965 December 6 - 21:05 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-4. LV Configuration: Scout X-4 S139R. -
FRANCE 1 Nation: France. Payload: FR 1. Mass: 60 kg (132 lb). Class: Earth. Type: Ionosphere. Spacecraft: FRANCE. Agency: CNES. Perigee: 696 km (432 mi). Apogee: 707 km (439 mi). Inclination: 75.90 deg. Period: 98.80 min. COSPAR: 1965-101A. USAF Sat Cat: 1814. VLF wave propagation studies. Investigation of the properties of the ionized layers of the atmosphere by observation of the propagation of the properties of very low frequency waves in the ionosphere. First registered by the United States in A/AC.105/INF.125. Orbit given there was 99 .9 min, 749 x 753 km x 75.9 deg, with note: France provided the payload for 1965-101A.
References: 2, 6.
1965 December 7 - Launch Site: Baikonur. Launch Complex: PU32. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 December 7 - 02:28 GMT - Launch Site: Johnston Island. Launch Complex: LE2. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2J. LV Configuration: Thor DSV-2J 188 (20011). -
AFP-437(AP) interceptor mission Nation: USA. Agency: USAF. Apogee: 487 km (302 mi). References: 2.
1965 December 7 - 03:53 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. -
ESRO C07 / 1 Aeronomy mission Nation: Europe. Agency: ESRO. Apogee: 150 km (90 mi). References: 2.
1965 December 8 - Launch Vehicle: Saturn V. -
Apollo J-2 engine captive-fired for 388 sec Nation: USA. Program: Apollo. An 889-kilonewton (200,000-lb) thrust J-2 engine was captive-fired for 388 sec on a new test stand at MSFC. The J-2 engine would be used to power the Saturn S-IVB stage for the Saturn V. Ten tests of the liquid hydrogen-liquid oxygen powered rocket engine had been conducted at MSFC since the J-2 engine test facility was put into use in August 1965.
References: 16.
1965 December 8 - -
Soyuz VI Nation: USSR. Spacecraft: Soyuz VI. Flight: Soyuz VI Flight 1, Gemini 7, Voskhod 3. Kamanin meets with an engineering delegation from Kuibyshev. They are seeking a close relationship with the cosmonaut cadre in development of the military reconnaissance version of Soyuz, which they are charged with developing. They have already been working with the IAKM for over a year in establishing he basic requirements. Kamanin finds this refreshing after the arms-length relationship with Korolev's bureau. Meanwhile Gemini 7 orbits above, and there is not the slightest word on the schedule for Volynov-Gorbatko's Voskhod 3 flight, which would surpass the new American record.
References: 376.
1965 December 8-10 - Launch Vehicle: Titan. Model: Titan 2. -
Gemini launch vehicle 9 was erected in the east cell of the vertical test facility at Martin-Baltimore. Nation: USA. Flight: Gemini 9. Power was applied to the launch vehicle for the first time on December 22, and Subsystems Functional Verification Tests were completed January 20, 1966.
1965 December 8 - 13:21 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3. LV Configuration: Black Brant III NC7.179. -
Aeronomy mission Nation: USA. Agency: NRL. Apogee: 140 km (80 mi). References: 2.
1965 December 9 - -
Voskhod 3 ECS trials Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3. The 15-day trial of the oxygen regeneration system for the long-duration Voskhod flights began at IMBP on 3 December. On 8 December Korolev ordered the test run extended to 20 days. The system has to maintain cabin temperature at 21 deg C, within a maximum range of 10 to 35 deg C. It produced 18 litres of oxygen per crew member per hour. In tests Volynov was found to consume 16.5 litres per hour, and Gorbatko 15.5 litres. But during intense activity these values can increase 5 to 6 times. Kamanin is particularly worried that in abort / high-G situations the system may prove inadequate.
References: 376.
1965 December 9-16 - -
Fire-till-touchdown not feasible for the Apollo LEM Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Preliminary results of the "fire-till-touchdown" study by Grumman indicated that this maneuver was not feasible. The engine might be exploded by driving the shock wave into the nozzles. Additional Details: Fire-till-touchdown not feasible for the Apollo LEM. References: 16.
1965 December 9-16 - -
Apollo Block II critical design review on the earth landing system Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Nine review item dispositions were submitted at the Block II critical design review concerning the earth landing system and shock attenuation system (struts). Six were on specifications, one on installation drawings, and two on capability. The two most significant were: - the contract for Block II parachutes had not been awarded and consequently top installation drawings were not yet available for review; and
- specifications defining crew couch strut loading tolerances had not been released but the strut drawings had.
References: 16.
1965 December 9 - 20:33 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun CRL AA6.173. -
Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 139 km (86 mi). References: 2.
1965 December 9 - 21:10 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 448 / Agena D SS-01B 1621. -
KH-4A 1027 Nation: USA. Payload: KH-4A s/n 1027 / Agena D 1621. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 186 km (115 mi). Apogee: 439 km (272 mi). Inclination: 80.10 deg. Period: 90.80 min. COSPAR: 1965-102A. USAF Sat Cat: 1816. Decay Date: 1965-12-26. KH-4A. Erratic attitude necessitated recovery after two days of operation. All cameras operated satisfactorily. References: 2, 6.
1965 December 10 - -
Apollo at-sea operational qualification tests completed Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. At-sea operational qualification tests, using boilerplate 29 to simulate spacecraft 009, were completed. All mechanical system components performed satisfactorily, except for the recovery flashing light. Additional Details: Apollo at-sea operational qualification tests completed. References: 16.
1965 December 10 - Launch Site: Green River. Launch Complex: Pad 1. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena C023. -
USAF C023 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1965 December 10 - 05:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun CRL AA6.174. -
Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 141 km (87 mi). References: 2.
1965 December 10 - 08:09 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. LV Configuration: Vostok 8A92 U15001-04. -
Cosmos 99 Nation: USSR. Payload: Zenit-2 11F61 s/n 32. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: MOM. Perigee: 203 km (126 mi). Apogee: 309 km (192 mi). Inclination: 65.00 deg. Period: 89.60 min. COSPAR: 1965-103A. USAF Sat Cat: 1817. Duration: 8.00 days. Decay Date: 1965-12-18. Area survey photo reconnaissance satellite. References: 2, 6,93.
1965 December 11 - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. Model: Nike Javelin. -
Aeronomy mission - 178 lb payload Nation: USA. Agency: USAF?. Apogee: 130 km (80 mi). References: 2.
1965 December 11 - 04:05 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. -
ESRO C07 / 2 Aeronomy mission Nation: Europe. Agency: ESRO. Apogee: 159 km (98 mi). References: 2.
1965 December 11 - 18:55 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache CRL AE5.558. -
Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 155 km (96 mi). References: 2.
1965 December 12 - Launch Vehicle: Titan. Model: Titan 2. -
Gemini 6 launch aborted. Nation: USA. Flight: Gemini 6. The scheduled launch of Gemini VI-A was aborted when the Master Operations Control Set automatically shut down the Gemini launch vehicle a second after engine ignition because an electrical umbilical connector separated prematurely. The launch was canceled at 9:54 a.m., e.s.t. Emergency procedures delayed raising the erector until 11:28, so the crew was not removed until 11:33 a.m. Launch was rescheduled for December 15. Routine analysis of the engine data, begun immediately after shutdown, revealed decaying thrust in one first stage engine subassembly before shutdown had been commanded. The problem was diagnosed as a restriction in the gas generator circuit of the subassembly, which would have caused shutdown about 1 second later than it actually occurred as a result of the umbilical disconnect. Source of the restriction proved to be a protective dust cap inadvertently left in place in the gas generator oxidizer injector inlet port. The anomalies were corrected and recycling, based on long-prepared contingency plans, proceeded without incident through launch on December 15.
1965 December 12 - -
Gemini 6 pad abort Nation: USA. Program: Gemini. Flight: Gemini 6, Gemini 7. The Titan 2 engines shut down a moment after ignition. The fault that caused the Titan to shut down saved the astronaut's lives; the quick thinking of the astronauts in not pulling the abort handles saved the mission.
1965 December 12 - 04:51 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache CRL AE5.172. -
Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 155 km (96 mi). References: 2.
1965 December 13 - 06:20 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-16. -
Ozone profile Ionosphere / aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 318 km (197 mi). References: 2.
1965 December 13 - 10:08 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL131. -
Solar X-rays / SpE / Li Ionosphere / solar x-rays mission Nation: Australia. Agency: WRE/RAE. Apogee: 130 km (80 mi). References: 2.
1965 December 14 - Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7A. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 1,350 km (830 mi). References: 2.
1965 December 14 - 12:49 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure CE-6. -
ESRO C06 / 1 Solar x-ray mission Nation: Europe. Agency: ESRO. Apogee: 159 km (98 mi). References: 2.
1965 December 14 - 17:20 GMT - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 516. -
Follow-on operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1965 December 15 -
1965 December 15 - Launch Vehicle: Saturn V.
1965 December 15 - -
Proposal for four additional Apollo LEMs Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Flight: Apollo 20. Grumman was invited to provide NASA with a cost-plus-incentive-fee proposal to provide four LEMs subsequent to LEM-11, with the proposal due at MSC by the close of business on the following day. The proposal should be based on a vehicular configuration similar to LEM-11 in all respects, including supporting activities, contractual provisions, and specifications applicable to LEM-11. The required shipment dates for the four vehicles would be December 13, 1968, February 11, 1969, April 11, 1969, and June 10, 1969, respectively.
References: 16.
1965 December 15 - 13:37 GMT - Launch Site: Cape Canaveral. Launch Complex: LC19. Launch Pad: -. Launch Vehicle: Titan. Model: Titan II GLV. LV Configuration: Titan II GLV GT-6 / 62-12561. -
Gemini 6 Nation: USA. Program: Gemini. Payload: Gemini SC6. Mass: 3,546 kg (7,817 lb). Class: Manned. Type: Spacecraft. Spacecraft: Gemini. Location of Spacecraft: McDonnell Planetarium, Saint Louis, MO. Agency: NASA MSC. Perigee: 258 km (160 mi). Apogee: 271 km (168 mi). Inclination: 28.90 deg. Period: 89.60 min. COSPAR: 1965-104A. USAF Sat Cat: 1839. Duration: 1.08 days. Decay Date: 1965-12-16. Crew: Schirra, Stafford. Flight: Gemini 6, Gemini 7. The primary objective of the mission, crewed by command pilot Astronaut Walter M. Schirra, Jr., and pilot Astronaut Thomas P. Stafford, was to rendezvous with spacecraft No. 7. Among the secondary objectives were stationkeeping with spacecraft No. 7, evaluating spacecraft reentry guidance capability, testing the visibility of spacecraft No. 7 as a rendezvous target, and conducting three experiments. After the launch vehicle inserted the spacecraft into an 87 by 140 nautical mile orbit, the crew prepared for the maneuvers necessary to achieve rendezvous. Four maneuvers preceded the first radar contact between the two spacecraft. The first maneuver, a height adjustment, came an hour and a half after insertion, at first perigee; a phase adjustment at second apogee, a plane change, and another height adjustment at second perigee followed. The onboard radar was turned on 3 hours into the mission. The first radar lock-on indicated 246 miles between the two spacecraft. The coelliptic maneuver was performed at third apogee, 3 hours 47 minutes after launch. The terminal phase initiation maneuver was performed an hour and a half later. Two midcourse corrections preceded final braking maneuvers at 5 hours 50 minutes into the flight. Rendezvous was technically accomplished and stationkeeping began some 6 minutes later when the two spacecraft were about 120 feet apart and their relative motion had stopped. Stationkeeping maneuvers continued for three and a half orbits at distances from 1 to 300 feet. Spacecraft No. 6 then initiated a separation maneuver and withdrew to a range of about 30 miles. The only major malfunction in spacecraft No. 6 during the mission was the failure of the delayed-time telemetry tape recorder at 20 hours 55 minutes ground elapsed time, which resulted in the loss of all delayed-time telemetry data for the remainder of the mission, some 4 hours and 20 minutes. The flight ended with a nominal reentry and landing in the West Atlantic, just 10 km from the planned landing point, on December 16. The crew remained in the spacecraft, which was recovered an hour later by the prime recovery ship, the aircraft carrier Wasp.Gemini 6 was to have been the first flight involving docking with an Agena target/propulsion stage. However the Agena blew up on the way to orbit, and the spacecraft was replaced by Gemini 7 in the launch order.
For lack of a target, NASA decided to have Gemini 6 rendezvous with Gemini 7. This would require a quick one week turnaround of the pad after launch, no problem with Russian equipment but a big accomplishment for the Americans. The first launch attempt was aborted; the Titan II ignited for a moment, then shut down and settled back down on its launch attachments. Schirra waited it out, did not pull the abort handles that would send the man catapulting out of the capsule on their notoriously unreliable ejection seats. The booster was safed; Schirra had saved the mission and the launch three days later went perfectly. The flight went on to achieve the first manned space rendezvous controlled entirely by the self-contained, on-board guidance, control, and navigation system. This system provided the crew of Gemini 6 with attitude, thrusting, and time information needed for them to control the spacecraft during the rendezvous. Under Schirra's typically precise command, the operation was so successful that the rendezvous was complete with fuel consumption only 5% above the planned value to reach 16 m separation from Gemini 7.
References: 2, 6, 26, 33,60.
1965 December 15 - 17:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.247UI. -
Electron density Ionosphere mission Nation: USA. Agency: NASA. Apogee: 184 km (114 mi). References: 2.
1965 December 15 - 19:19 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.68II. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 185 km (114 mi). References: 2.
1965 December 16 - -
Space race Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Gemini 6, Gemini 7, Voskhod 3. Gemini 7 has the space flight duration record, and Gemini 6 has achieved the first rendezvous in orbit. Yesterday Pashkov sent a letter to Smirnov, asking that new series of Voskhod spacecraft be ordered as insurance in case of further delays in development of the Soyuz spacecraft. Kamanin believes he sees panic setting in with the leadership. The next day Kamanin attempts to call Korolev, only to find he is out sick.
References: 376.
1965 December 16 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C94. -
Aeronomy mission Nation: France. Agency: CNES. Apogee: 150 km (90 mi). References: 2.
1965 December 16 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C128. -
Ionosphere mission Nation: France. Agency: CNES. Apogee: 150 km (90 mi). References: 2.
1965 December 16 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C131. -
Ionosphere mission Nation: France. Agency: CNES. Apogee: 150 km (90 mi). References: 2.
1965 December 16 - Launch Site: Vandenberg. Launch Complex: LF24. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2017. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1965 December 16 - Launch Site: Baikonur. Launch Complex: LC67/21. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36-O. LV Configuration: R-36O 8K69 U22502 No. 1L. -
OGCh No. 01L Nation: USSR. Mass: 1,700 kg (3,700 lb). Spacecraft: OGCh. Agency: RVSN. Apogee: 200 km (120 mi). COSPAR: U651216A. First suborbital test of the FOBS system. Impacted within specification CEP in target zone. References: 2, 279.
1965 December 16 - 07:31 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta E. LV Configuration: Thor Delta E 460/D35. -
Pioneer 6 Nation: USA. Program: Pioneer. Payload: Pioneer A. Mass: 63 kg (138 lb). Class: Solar. Spacecraft: Pioneer 6-7-8-9-E. Agency: NASA ARC. COSPAR: 1965-105A. USAF Sat Cat: 1841. Measured solar wind, Sun's magnetic field. Solar Orbit (Heliocentric). Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1965 December 16 - -
Landing of Gemini 6 Nation: USA. Program: Gemini. Flight: Gemini 6, Gemini 7. Gemini 6 splashed down near the aircraft carrier Wasp at 15:28 GMT. The capsule was lifted to the carrier deck with the crew aboard. When the hatch doors were opened, the spacemen gave the thumbs-up while the Navy band crashed in with 'Anchors Aweigh'. It was the first recovery carried live via satellite television.
1965 December 17 - 02:24 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M. LV Configuration: Vostok 8A92M R15000-31. -
Cosmos 100 Nation: USSR. Payload: Meteor no. 3. Mass: 4,730 kg (10,420 lb). Class: Earth. Type: Weather. Spacecraft: Meteor. Agency: MOM. Perigee: 485 km (301 mi). Apogee: 547 km (339 mi). Inclination: 65.00 deg. Period: 95.00 min. COSPAR: 1965-106A. USAF Sat Cat: 1843. Decay Date: 2002-02-15. Probable weather satellite. Investigation of the upper atmosphere and outer space. References: 2, 6.
1965 December 18 - -
VPK Emergency Meeting Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Gemini 6, Gemini 7, Voskhod 3, , Voskhod 4, Voskhod 5, Voskhod 6. Smirnov calls the Military Industrial Commission and the Chief Designers together to consider Pashkov's letter and how to respond to the American Gemini successes. Korolev is ill and unable to attend. His deputies are unable to provide any firm schedule for completion and fight of Voskhod or Soyuz spacecraft. Soviet projections are that over the next year the Americans will fly manned missions of 20 to 30 days duration and conduct many military experiments from manned spacecraft. It is decided that a crash effort needs to be applied to Soyuz development. However no further Voskhods will be built beyond the five already being assembled, but those Voskhods will be dedicated to setting record duration flights of 15 to 30 days and conducting military experiments.
References: 376.
1965 December 18 - 04:59 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.69II. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 188 km (116 mi). References: 2.
1965 December 18 - 06:00 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-17. -
Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 316 km (196 mi). References: 2.
1965 December 18 - -
Landing of Gemini 7 Nation: USA. Program: Gemini. Flight: Gemini 7. Gemini 7 landed at 14:05 GMT only 11.8 km from the target point after a record 14 day mission..
1965 December 19 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. FAILURE: Failure. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1965 December 20 - Launch Vehicle: N1. -
Decision to use analogue guidance in early N1 launches Nation: USSR. Program: Lunar L3. Spacecraft: LK, Soyuz 7K-LOK. Pilyugin called Keldysh to tell him he had heard that Keldysh again wanted to form an expert commission to study guidance system development problems with the N1, with Bushuyev as the head. Additional Details: Decision to use analogue guidance in early N1 launches. References: 367.
1965 December 20 - -
Falling behind Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Gemini 7, Voskhod 3, Voskhod 4, Voskhod 5, Soyuz 1, Soyuz 2A, Soyuz 7K-L1 mission 1. Gemini 7 has landed. The Americans achieved every manned spaceflight objective they had set for themselves in 1965, and made 50% more launches than the Soviet Union. On the other side, the Russians have only been able to fly Voskhod 2. Korolev promised that three Voskhod and two Soyuz spacecraft would be completed in 1965, and that two of each would fly before November 7. The year has ended, and not a single spacecraft has been delivered. Kamanin calls Korolev, who says that the unfinished Voskhods will not be completed, and that the four completed spacecraft will be used for long-duration flights. All of his bureau's energies will be concentrated on developing Soyuz spacecraft to perfect space docking and to perform lunar flyby missions.
References: 376.
1965 December 20 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C130. -
Ionosphere mission Nation: France. Agency: CNES. Apogee: 150 km (90 mi). References: 2.
1965 December 20 - 13:39 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 85D. -
NTMP KX-31 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi). References: 2.
1965 December 20 - 16:33 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-188. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1965 December 21 - -
Robert C Seamans, Jr becomes Deputy Administrator of NASA Nation: USA. Program: Apollo. Robert C. Seamans, Jr., was sworn in as Deputy Administrator of NASA, succeeding Hugh L. Dryden who died December 2. Seamans would also retain his present position as Associate Administrator for an indefinite period of time.NASA Administrator James E. Webb administered the oath of office. He had announced in Austin, Tex., on December 10, that President Lyndon B. Johnson had accepted his recommendation that Seamans be named to the number two NASA post.
References: 16.
1965 December 21 - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7A. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 1,350 km (830 mi). References: 2.
1965 December 21 - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3C. LV Configuration: Titan IIIC 3C-8. -
Transtage 8 Nation: USA. Spacecraft: OV2. Agency: USAF AFSC. COSPAR: 1965-108xx. USAF Sat Cat: 1863. Decay Date: 1975-08-17. References: 2, 279.
1965 December 21 - 06:14 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. -
Cosmos 101 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 4. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 256 km (159 mi). Apogee: 533 km (331 mi). Inclination: 48.80 deg. Period: 92.50 min. COSPAR: 1965-107A. USAF Sat Cat: 1846. Completed Operations Date: 1966-03-11. Decay Date: 1966-07-12. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1965 December 21 - 14:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3C. LV Configuration: Titan IIIC 3C-8. -
OV2-03 Nation: USA. Mass: 193 kg (425 lb). Class: Earth. Type: Magnetosphere. Spacecraft: OV2. Agency: USAF. Perigee: 321 km (199 mi). Apogee: 22,846 km (14,195 mi). Inclination: 26.80 deg. Period: 399.30 min. COSPAR: 1965-108A. USAF Sat Cat: 1863. Decay Date: 1975-08-17. Upper stage separation failed. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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LES 4 Nation: USA. Mass: 52 kg (114 lb). Class: Technology. Type: Comsat. Spacecraft: LES. Agency: USAF. Perigee: 189 km (117 mi). Apogee: 33,632 km (20,897 mi). Inclination: 26.60 deg. Period: 589.20 min. COSPAR: 1965-108B. USAF Sat Cat: 1870. Decay Date: 1977-08-01. Lincoln Experimental Satellite; experimental commsat; transmitted in X-band. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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Oscar 4 Nation: USA. Program: Oscar. Mass: 13 kg (28 lb). Class: Communications. Type: Amateur Radio. Spacecraft: Oscar. Agency: OSCAR. Perigee: 162 km (100 mi). Apogee: 33,549 km (20,846 mi). Inclination: 26.80 deg. Period: 587.50 min. COSPAR: 1965-108C. USAF Sat Cat: 1902. Decay Date: 1976-04-12. OSCAR IV was launched piggyback with three United States Air Force satellites. The launch vehicle had a partial failure and placed the spacecraft in a low orbit preventing widespread amateur use. Orbit 29120 x 168 km. Inclination 26.8 degrees. Period 587.5 minutes. Weight 18.1 kg. Four monopole antennas. OSCAR IV was built by the TRW Radio Club of Redondo Beach, California. It had a 3 Watt 10 kHz wide linear transponder (144 MHz uplink and 432 MHz downlink). In operation until March 16, 1966. Re-entry April 12, 1976. Total operation 85 days. OSCAR IV provided the first US-Soviet amateur link.
References: 2, 6.
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LES 3 Nation: USA. Mass: 16 kg (35 lb). Class: Technology. Type: Comsat. Spacecraft: LES. Agency: USAF. Perigee: 267 km (165 mi). Apogee: 4,829 km (3,000 mi). Inclination: 26.50 deg. Period: 139.90 min. COSPAR: 1965-108D. USAF Sat Cat: 1941. Decay Date: 1968-04-06. Radio signal source for commsat tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1965 December 22 - -
Kamanin and Korolev clash Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3. The two have a difficult discussion over crewing for Voskhod 3. Korolev has found that Katys has been taken out of training for the mission. He does not agree with Kamanin's all-military pilot crew of Volynov and Gorbatko. Kamanin is tired of Korolev's caprices and his endless fighting with Glushko, Pilyugin, Voronin, Kosberg, and other chief designers. Korolev has had it with the military excluding civilians and civilian objectives from manned space.
References: 376.
1965 December 22 - 04:33 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout A. LV Configuration: Scout A S140C. -
Transit O-6 Nation: USA. Program: Transit. Mass: 60 kg (132 lb). Class: Navigation. Spacecraft: Transit. Agency: USN. Perigee: 891 km (553 mi). Apogee: 1,059 km (658 mi). Inclination: 89.10 deg. Period: 104.60 min. COSPAR: 1965-109A. USAF Sat Cat: 1864. Spacecraft built by Naval Avionics Facility, but refurbished by APL. Operated for 7 to 11 months, but then failed due to poor workmanship of NAFI components. References: 2, 6.
1965 December 22 - 14:10 GMT - Launch Site: Vandenberg. Launch Complex: 395-C. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-73. -
Sea Rover operational test Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1965 December 23 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Jericho. FAILURE: Failure. -
Test mission Nation: Israel. Agency: Dassault. Apogee: 100 km (60 mi). References: 2.
1965 December 23 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: LC41/4?. Launch Vehicle: R-16. Model: R-16U. -
Military training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1965 December 24 - -
Barwell Meteorite Fall (Hit Car, Buildings) Nation: UK.
1965 December 24 - 21:06 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 451 / Agena D SS-01B 1610. -
KH-4A 1028 Nation: USA. Payload: KH-4A s/n 1028 / Agena D 1610. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 181 km (112 mi). Apogee: 443 km (275 mi). Inclination: 80.00 deg. Period: 90.70 min. COSPAR: 1965-110A. USAF Sat Cat: 1866. Decay Date: 1966-01-20. KH-4A. Cameras operated satisfactorily. References: 2, 6.
1965 December 25 - Launch Site: Baikonur. Launch Complex: LC41/3. Launch Pad: LC41/3?. Launch Vehicle: R-16. Model: R-16U. -
Military training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1965 December 25 - Launch Site: Baikonur. Launch Complex: PU33. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 December 25 - Launch Site: Baikonur. Launch Complex: PU32. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 December 26 - Launch Site: Baikonur. Launch Complex: LC41/3. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Military training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1965 December 26 - Launch Site: Baikonur. Launch Complex: PU31. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1965 December 27 - 22:19 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 11A510. LV Configuration: Soyuz 11A510 G15000-01. -
Cosmos 102 Nation: USSR. Program: RORSAT. Mass: 3,800 kg (8,300 lb). Class: Surveillance. Type: Naval Radarsat. Spacecraft: US-A. Agency: MOM. Perigee: 205 km (127 mi). Apogee: 267 km (165 mi). Inclination: 64.90 deg. Period: 89.20 min. COSPAR: 1965-111A. USAF Sat Cat: 1867. Decay Date: 1966-01-13. Prototype RORSAT hardware using chemical batteries in place of nuclear reactor. References: 2, 6, 290.
1965 December 28 - Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. FAILURE: First stage failed. -
DS-K-40 s/n 1 Nation: USSR. Program: DS. Payload: DS-K-40. Class: Technology. Spacecraft: DS-K-40. Agency: RVSN. COSPAR: F651228A. Development of systems for the later operational Tselina satellites. References: 2.
1965 December 28 - 12:30 GMT - Launch Site: Baikonur. Launch Complex: LC41/15. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 65S3. LV Configuration: Kosmos 65S3 09LP. -
Cosmos 103 Nation: USSR. Program: Strela. Mass: 875 kg (1,929 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-2. Agency: MO SSSR. Perigee: 176 km (109 mi). Apogee: 179 km (111 mi). Inclination: 56.00 deg. Period: 88.00 min. COSPAR: 1965-112A. USAF Sat Cat: 1868. Decay Date: 1990-01-02. Possible test flight. References: 2, 6, 279.
1965 December 29 - -
NASA support to the Air Force on the MOL summarized. Nation: USA. Spacecraft: MOL. In the initial activity report outlining MSC's support to the Air Force on the MOL, Gemini Program Manager Charles W. Mathews summarized activity to date. He cited receipt on 20 November 1965 of authority to transfer surplus Gemini equipment to the MOL project. Since that time, he said, MSC had delivered to the Air Force several boilerplate test vehicles and a variety of support and handling equipment. MOL program officials and astronauts had also visited Houston for technical discussions and briefings.
1965 December 30 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. FAILURE: Failure. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1965 December 31 - -
Apollo SM reaction control system engine qualification completed Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The SM reaction control system engine qualification was completed with no apparent failures. References: 16.
1965 December 31 - Launch Vehicle: N1. Model: N1 1964. -
Daunting year ahead Nation: USSR. Program: Voskhod, Soyuz, Lunar L1. Spacecraft: Soyuz 7K-OK, Soyuz 7K-L1, Soyuz 7K-LOK, LK. Flight: Soyuz 1, Soyuz 2A, Soyuz 7K-L1 mission 1, Soviet Lunar Landing. Kamanin looks ahead to the very difficult tasks scheduled for 1966. There are to be 5 to 6 Soyuz flights, the first tests of the N1 heavy booster, the first docking in space. Preparations will have to intensify for the first manned flyby of the moon in 1967, following by the planned first Soviet moon landing in 1967-1969. Kamanin does not see how it can all be done on schedule, especially without a reorganization of the management of the Soviet space program.
References: 376.
1965 December - -
16 flights made in the Apollo LLRV Nation: USA. Program: Apollo. Spacecraft: Apollo LLRV. During the month 16 flights were made in the LLRV. Of these, 11 were devoted to concluding the handling qualities evaluation of the rate- command vehicle attitude control system. The other five flights were required to check out a new pilot, Lt. Col. E. E. Kluever of the Army, who would participate in the remaining research flight testing performed on the LLRV at Flight Research Center. On December 15 the craft was grounded for cockpit modifications which would make the pilot display and controllers more like those of the LEM.
References: 16.
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