1966 January 1 - -
Study grants for AAP astonomical instrumentation to be flown in the 1969-1975 period. Nation: USA. Spacecraft: Orbital Workshop. Homer E. Newell, Associate Administrator for Space Science and Applications, announced opportunities for study grants to competent astronomers for conceptual and preliminary design work leading to instrumentation to be flown in the 1969-1975 period. A description of the Apollo telescope mount was included.
1966 - Launch Vehicle: R-16, R-5, Soyuz. -
Twelfth Directorate nuclear weapons units an integrated part operational rocket field units Nation: USSR. Up to 1965 the warheads were still stored separately form Soviet ballistic missiles. This was changed so that the individual nuclear weapons units were made an integrated part of the operational rocket field units.
1966 - Launch Site: Kapustin Yar. Launch Complex: PL87. Launch Pad: -. Launch Vehicle: RT-2. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1966 January - -
Dynasoar 1 Nation: USA. Spacecraft: Dynasoar. Prior to cancellation of the Dynasoar project, the first unmanned flight was planned for the fourth flight test of the Titan 3C booster. References: 152.
1966 January - -
HL-10 delivered to NASA Nation: USA. Spacecraft: HL-10. During the next 10 months it was instrumented for the research program and prepared for flight. The HL-10 and the M2-F2 were tested in wind tunnels at Ames Research Center before research flights began.
1966? - Launch Site: Ile du Levant. Launch Complex: Nemo. Launch Pad: -. Launch Vehicle: MSBS. Model: MSBS M112. -
Caisson 2 test Nation: France. Agency: DMA. Apogee: 50 km (31 mi). References: 2.
1966 January 3-7 - -
Preliminary Design Review for the Apollo Block II pressure garment Nation: USA. Program: Apollo. Spacecraft: Apollo CSM, A7L. The Preliminary Design Review for the Block II pressure garment assembly was held at International Latex Corporation. References: 16.
1966 January 4 - Launch Vehicle: DF-4. -
Chinese ICBM plans Nation: China. Tsien proposes to add electronic countermeasures and other penetration aids to the DF-5 ICBM in order to defeat the planned American ABM system.
1966 January 4 - -
Korolev visits Cosmonaut Training Center Nation: USSR. Korolev visits the centre, and spends more than six hours with the cosmonauts. However he says nothing about concrete flight plans. Afterwards Kamanin meets with Gagarin, Titov, Popovvich, Nikolayev, Tereshkova, Bykovsky, Komarov, and Belyayev (Leonov is at courses at the Academy). A profound pessimism prevails. Nothing has come of the letter to Brezhnev.
References: 376.
1966 January 5 - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 461. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1966 January 6-13 - Launch Vehicle: Saturn V. -
Apollo Block I SPS engine tested to 600 seconds Nation: USA. Program: Apollo. The 500-second limitation for the Block I service propulsion system SPS engine qualification program was increased to 600 seconds for the last three altitude qualification tests. The spacecraft 020 SPS mission duty cycle required a 310-second burn and a 205-second burn. Discussions with Systems Engineering Division indicated that the long SPS burns were needed to support a full-duration S-IVB mission and there was little likelihood the requirement could be modified. The Block II engine delivery schedules prohibited obtaining a Block II engine in time to support spacecraft 020.
References: 16.
1966 January 7 - 08:24 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. -
Cosmos 104 Nation: USSR. Payload: Zenit-2 11F61 s/n 36. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: MOM. Perigee: 195 km (121 mi). Apogee: 379 km (235 mi). Inclination: 65.00 deg. Period: 90.20 min. COSPAR: 1966-001A. USAF Sat Cat: 1903. Duration: 8.00 days. Decay Date: 1966-01-15. Area survey photo reconnaissance satellite. Program not completely met. Spacecraft put into incorrect orbit by abnormal function of second and third stages of booster. References: 2, 6,93.
1966 January 8 - -
Space trainers Nation: USSR. Program: Voskhod, Soyuz. Spacecraft: Voskhod, Soyuz 7K-OK. Flight: Voskhod 3, Voskhod 4, Voskhod 5, Soyuz 1, Soyuz 2A. Tyulin and Mozzhorin review space simulators at TsPK. The 3KV and Volga trainers are examined. Tyulin believes the simulators need to be finished much earlier, to be used not just to train cosmonauts, but as tools for the spacecraft engineers to work together with the cosmonauts in establishing the cabin arrangement. This was already done on the 3KV trainer, to establish the new, more rational Voskhod cockpit layout. Tyulin reveals that the female Voskhod flight now has the support of the Central Committee and Soviet Ministers. He also reveals that MOM has promised to accelerate things so that four Voskhod and five Soyuz flights will be conducted in 1966. For 1967, 14 manned flights are planned, followed by 21 in 1968, 14 in 1969, and 20 in 1970. This adds up to 80 spaceflights, each with a crew of 2 to 3 aboard. Tyulin also supports the Kamanin position on other issues - the Voskhod ECS should be tested at the VVS' IAKM or Voronin's factory, not the IMBP. The artificial gravity experiment should be removed from Voskhod and replaced by military experiments. He promises to take up these matters with Korolev.
References: 376.
1966 January 8-11 - -
First Apollo fuel cell system test at White Sands Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The first fuel cell system test at White Sands Test Facility was conducted successfully. Primary objectives were: 1 to verify the capability of the ground support equipment and operational checkout procedure to start up, operate, and shut down a single fuel cell power plant; and 2 to evaluate fuel cell operations during cold gimbaling of the service propulsion engine.
References: 16.
1966 January 8 - 04:48 GMT - Launch Site: Vandenberg. Launch Complex: SLC10W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Burner 1. LV Configuration: Thor Burner 1 251. FAILURE: Second stage failed. -
DMSP-Block-4A F5 Nation: USA. Program: DMSP. Payload: DAPP 14/OPS 2394. Mass: 130 kg (280 lb). Class: Earth. Type: Weather. Spacecraft: DMSP Block 4A. Agency: U.S. Air Force. COSPAR: F660108A. Decay Date: 1966-01-06. Defense Meteorological Satellite Program. References: 126.
1966 January 8 - 13:11 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C103 TERLS-35. -
ISRO 15.03 Aeronomy / ionosphere mission Nation: India. Agency: ISRO. Apogee: 150 km (90 mi). References: 2.
1966 January 10 - -
Korolev hospitalised Nation: USSR. Korolev is in the hospital, requiring an operation on his colon. It is not expected to be difficult, although it carries some risk like all surgeries. He is expected to be in the hospital for two to three weeks. References: 376.
1966 January 10 - 17:14 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.248UI. -
Electron density Ionosphere mission Nation: USA. Agency: NASA. Apogee: 186 km (115 mi). References: 2.
1966 January 11 - -
Female flight go-ahead Nation: USSR. Program: Voskhod. Spacecraft: Voskhod, Berkut. Flight: Voskhod 5. Tyulin has ordered the crew for the female Voskhod flight to enter final flight training and the preparation of all necessary space suits, cabin uniforms, crew couch liners, documentation, and other final preparations. References: 376.
1966 January 12 - 14:00 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Boosted Dart. LV Configuration: Boosted Dart EXAMETNET 1. -
04 CNAE 6601 Aeronomy mission Nation: USA. Agency: CNAE. Apogee: 60 km (37 mi). References: 2.
1966 January 13 - Launch Vehicle: Saturn I. Model: Saturn IB. -
Land impact program for the Apollo CM Block I deleted Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. A decision made at a Program Management Review eliminated the requirement for a land impact program for the CM to support Block I flights. Post-abort CM land impact for Saturn IB launches had been eliminated from Complex 37 by changes to the sequence timers in the launch escape system abort mode. The Certification Test Specification and related Certification Test Requirements would reflect the new Block II land impact requirements.
References: 16.
1966 January 13 - Launch Site: Kwajalein. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. -
Interceptor mission Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2.
1966 January 13 - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: HIBEX. LV Configuration: HIBEX 10. -
10 test Nation: USA. Agency: USA/ARPA. Apogee: 20 km (12 mi). References: 2.
1966 January 14 - Launch Vehicle: N1. -
Korolev's death Nation: USSR. Program: Voskhod, Soyuz, Lunar L1. Spacecraft: Voskhod, Soyuz 7K-OK. Korolev dies at age 59 during what was expected to be routine colon surgery in Moscow. The day began for Kamanin with firm plans finally in place for the next three Voskhod and first three Soyuz flights. Volynov and Shonin will be the crew for the first Voskhod flight, with Beregovoi and Shatalov as their back-ups. That will be followed by a female flight of 15-20 days, with the crew begin Ponomaryova and Solovyova, with their back-ups Sergeychik (nee Yerkina) and Pitskhelaura (nee Kuznetsova). Tereshkova will command the female training group. Training is to be completed by March 15. After this Kamanin goes to his dacha, only to be called by General Kuznetsov around 19:00, informing him that Korolev has died during surgery. Kamanin does not minimise Korolev's key role in creating the Soviet space program, but believes the collectives can continue the program without him. In truth, Kamanin feels Korolev has made many errors of judgment in the last three years that have hurt the program. Mishin, Korolev's first deputy, will take over management of Korolev's projects. Kamanin feels that Mishin is a clever and cultured engineer, but he is no Korolev. Over the next three days the cosmonauts console Korolev's widow. Korolev's surgery was done personally by Petrovskiy, the Minister of Health. Korolev was told the surgery would take only a few minutes, but after five hours on the operating table, his body could no longer endure the insult, and he passed away.
References: 376.
1966 January 16 - -
National Academy of Sciences report outlining research objectives in lunar and planetary exploration for the 1970s and early 1980s. Nation: USA. Program: Skylab. Spacecraft: Viking. The Space Science Board of the National Academy of Sciences issued a report outlining research objectives in lunar and planetary exploration for the 1970s and early 1980s. The report affirmed earlier recommendations by the Space Science Board to NASA that unmanned exploration of Mars should have first priority in the post- Apollo space era. Secondary importance was assigned to detailed investigation of the lunar surface and to unmanned Venus probes. Clearly, the report reflected a predominant mood within the scientific community that scientific research in space take predominance over manned programs whose chief objectives, said the report, were 'other than scientific.'
Additional Details: National Academy of Sciences report outlining research objectives in lunar and planetary exploration for the 1970s and early 1980s..
1966 January 17 - 16:42 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-393. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 January 17 - 17:56 GMT - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C127. -
Ionosphere mission Nation: France. Agency: CNES. Apogee: 124 km (77 mi). References: 2.
1966 January 17 - 22:39 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.262CM. -
Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 206 km (128 mi). References: 2.
1966 January 18 - -
Korolev buried in Red Square Nation: USSR. The urn with Korolev's ashes is placed in the Kremlin Wall by an honor guard of cosmonauts and the highest leaders of the state. Kamanin knows that the like of Korolev will not be seen again. There are dozens of Chief Designers, but none with the genius, talent, and drive of Korolev. Kamanin worries for the future in the space race with the Americans. Even in life, Korolev was never able to achieve more than one or two spaceflights per year. Now, in 1966, they are supposed to achieve four times that flight rate without him.
References: 376.
1966 January 18 - Launch Site: Vandenberg. Launch Complex: LF26. Launch Pad: LF26?. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2053. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1966 January 18 - 00:32 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.263CM. -
TMA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 205 km (127 mi). References: 2.
1966 January 18 - 02:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.264CM. -
TMA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 167 km (103 mi). References: 2.
1966 January 18 - 03:19 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.90GG. -
Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 134 km (83 mi). References: 2.
1966 January 18 - 05:12 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.265CM. -
TMA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 207 km (128 mi). References: 2.
1966 January 18 - 11:31 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.266CM. -
Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 213 km (132 mi). References: 2.
1966 January 18 - 18:11 GMT - Launch Site: Johnston Island. Launch Complex: LE2. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2J. LV Configuration: Thor DSV-2J 242. -
AFP-437(AP) interceptor mission Nation: USA. Agency: USAF. Apogee: 459 km (285 mi). References: 2.
1966 January 19 - 20:10 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3 Agena D. LV Configuration: SLV-3 Agena D 7114 / Agena D 7114. -
KH 7-24 Nation: USA. Payload: KH-7 no. 24. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-7. Agency: NRO/USAF. Perigee: 138 km (85 mi). Apogee: 259 km (160 mi). Inclination: 93.80 deg. Period: 88.40 min. COSPAR: 1966-002A. USAF Sat Cat: 1939. Decay Date: 1966-01-25. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
-
OPS 3179/Agena D Nation: USA. Payload: Agena Pickaback. Mass: 60 kg (132 lb). Class: Sigint. Spacecraft: SSF. Agency: USAF. Perigee: 120 km (70 mi). Apogee: 149 km (92 mi). Inclination: 93.80 deg. Period: 87.20 min. COSPAR: 1966-002B. USAF Sat Cat: 1940. Decay Date: 1966-01-23. Not identified as a subsatellite ferret by McDowell. References: 2, 6, 172, 278.
1966 January 20 - -
Little Joe II A-004 Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Apollo Mission A-004 was successfully accomplished at White Sands Missile Range. This was the first flight test utilizing the Apollo Block I type spacecraft and the sixth and final test of the Apollo CSM development program at WSMR. Additional Details: Little Joe II A-004. References: 16.
1966 January 20 - 15:17 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Little Joe II. Model: Little Joe II 5-2-2. LV Configuration: Little Joe II-5-2-2 LJII-5 (12-51-3). -
Apollo A-004 Nation: USA. Agency: NASA. Apogee: 23 km (14 mi). References: 2.
1966 January 21 - Launch Site: Green River. Launch Complex: Pad 2. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena C025. -
USAF C025 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1966 January 21 - 08:14 GMT - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 1. LV Configuration: Dragon D-21. -
FU-133 Sodium release Aeronomy mission Nation: France. Agency: CNES. Apogee: 500 km (310 mi). References: 2.
1966 January 22 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2022. -
Force modification test Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1966 January 22 - 08:38 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. -
Cosmos 105 Nation: USSR. Payload: Zenit-2 11F61 s/n 38. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: MOM. Perigee: 203 km (126 mi). Apogee: 311 km (193 mi). Inclination: 65.00 deg. Period: 89.60 min. COSPAR: 1966-003A. USAF Sat Cat: 1945. Duration: 8.00 days. Decay Date: 1966-01-30. Area survey photo reconnaissance satellite. References: 2, 6,93.
1966 January 24 - -
New space schedules 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. The VVS General Staff reviews a range of documents, authored by Korolev before his death, and supported by ministers Afanasyev and Petrovskiy. The schedules for the projects for flying around and landing on the moon are to be delayed from 1966-1967 to 1968-1969. A range of other space programs will similarly be delayed by 18 to 24 months. An institute for tests of space technology will be established at Chelomei's facility at Reutov. The IMBP will be made the lead organization for space medicine. Responsibility for space technology development will be moved from MOM to 10 other ministries. 100 million roubles have been allocated for the establishment of new research institutes. Kamanin is appalled, but Malinovskiy favours getting rid of the responsibility for these projects. The arguments over these changes - which reduce the VVS role in spaceflight - will be the subject of much of Kamanin's diary over the following weeks.
References: 376.
1966 January 24 - 05:42 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.185GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 125 km (77 mi). References: 2.
1966 January 25 - Launch Site: White Sands. Launch Complex: LC50. Launch Pad: -. Launch Vehicle: Sprint. LV Configuration: Sprint ABM FLA-2. FAILURE: Failure. -
Test mission Nation: USA. Agency: USA. Apogee: 0 km ( mi). References: 2.
1966 January 25 - 01:52 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.158UA. -
Spheres Aeronomy mission Nation: USA. Agency: NASA. Apogee: 167 km (103 mi). References: 2.
1966 January 25 - 12:28 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 106 Nation: USSR. Program: DS. Payload: DS-P1-I s/n 1. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-I. Agency: MO SSSR. Perigee: 281 km (174 mi). Apogee: 553 km (343 mi). Inclination: 48.40 deg. Period: 92.80 min. COSPAR: 1966-004A. USAF Sat Cat: 1949. Completed Operations Date: 1966-11-15. Decay Date: 1966-11-14. Operational radar target for the ABM forces. References: 2, 6, 99.
1966 January 26 - 02:10 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: S-250. LV Configuration: S-250 BT-250-1. -
Test mission Nation: Japan. Agency: ISAS. Apogee: 6.00 km (3.70 mi). References: 2.
1966 January 26 - 10:32 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 176. -
Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi). References: 2.
1966 January 26 - 23:50 GMT - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. -
Sandia 154-60 Aeronomy mission Nation: USA. Agency: Sandia. Apogee: 110 km (60 mi). References: 2.
1966 January 27 - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1243. -
Follow-on operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1966 January 27 - 01:29 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NRL NC3.186. -
Aeronomy / ionosphere mission Nation: USA. Agency: NRL. Apogee: 243 km (150 mi). References: 2.
1966 January 28 - -
OKB-1 Program Review Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3. Kamanin, Gagarin, Komarov, and other VVS staff attend the first program review held since Korolev's death. Mishin reviews spacecraft build status. Voskhod s/n 5 is to be shipped to Tyuratam on 1 February and launched in the first half of February. This is the spacecraft fitted for the 30-day unmanned biosat mission with dogs. Kamanin had argued with Korolev over the last year that this flight was unnecessary, but Korolev did not want to expose the cosmonauts to the risk of a long-duration spaceflight with a heavily modified spacecraft without an unmanned precursor flight. The manned flight of Voskhod s/n 6 on an 18-day mission can only begin after the landing of s/n 5, e.g. launch in the period 10-20 March.
References: 376.
1966 January 28 - 17:06 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout A. LV Configuration: Scout A S142C. -
Transit O-7 Nation: USA. Program: Transit. Mass: 50 kg (110 lb). Class: Navigation. Spacecraft: Transit. Agency: USN. Perigee: 850 km (520 mi). Apogee: 1,180 km (730 mi). Inclination: 90.00 deg. Period: 105.40 min. COSPAR: 1966-005A. USAF Sat Cat: 1952. Naval Avionics Facility-assembled production spacecraft. Failed after a few weeks operation. References: 2, 6.
1966 January 31 - -
Voskhod sinks from sight Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3, Voskhod 4, Voskhod 5. After Korolev's death, the leadership simply "forgets" about the instructions to fly a new series of Voskhods. The decrees ordering the flights are never rescinded, but the issue is not seriously raised again. References: 367.
1966 January 31 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-388. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 January 31 - 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.
1966 January 31 - 11:41 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M U103-32. -
Luna 9 Nation: USSR. Program: Luna. Payload: E-6M s/n 13. Mass: 1,580 kg (3,480 lb). Class: Planetary. Type: Lunar. Spacecraft: Luna E-6. Agency: MOM. COSPAR: 1966-006A. USAF Sat Cat: 1954. Decay Date: 1966-02-03. Soft landed on Moon; photographed surface for 3 days. Landed on Moon 3 February 1966 at 18:44:52 GMT, Latitude 7.08 N, Longitude 295.63 E - Oceanus Procellarum. The Luna 9 spacecraft was the first spacecraft to achieve a lunar soft landing and to transmit photographic data to Earth. Seven radio sessions, totaling 8 hours and 5 minutes, were transmitted as were three series of TV pictures. When assembled, the photographs provided a panoramic view of the nearby lunar surface. The pictures included views of nearby rocks and of the horizon 1.4 Km away from the spacecraft.
References: 2, 6, 64, 296.
1966 February 1 - Launch Site: Baikonur. Launch Complex: LC110L. Launch Pad: -. Launch Vehicle: N1. -
Construction starts on N1 launch pad 110 west. Nation: USSR. Program: Lunar L3. References: 96.
1966 February - -
Douglas summary report covering the activities of three phases of the MORL study. Nation: USA. Spacecraft: MORL. Douglas Aircraft Company submitted a summary report to LaRC covering the activities of three phases of the MORL study. General objectives of the MORL study were to (1) establish the feasibility of a manned research laboratory; (2) determine the required level of technical, logistic, and economic support; and (3) define a realistic space station program responsive to the needs of NASA and other government agencies in particular and the scientific community in general. The three phases of the study were Phase I (June-September 1963)-System Comparison and Selection Study of a MORL Phase IIa (December 1963-November 1964)-Optimization of the MORL System Concept Phase IIb (December 1964-February 1966)-Development of the MORL System Utilization Potential.
Additional Details: Douglas summary report covering the activities of three phases of the MORL study..
1966 February 1 - 18:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NRL NE3.156R. -
Spectroheliograph Solar soft x-ray mission Nation: USA. Agency: NRL. Apogee: 209 km (129 mi). References: 2.
1966 February 1 - 20:11 GMT - Launch Site: Point Barrow. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.182GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 117 km (72 mi). References: 2.
1966 February 1 - 20:46 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.147GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 118 km (73 mi). References: 2.
1966 February 2 - -
Voskhod parachute system Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3. Smirnov again questions the chief designers about the reliability of the parachute systems developed by Tkachev. The VVS remains troubled as to the reliability of these systems. Recently the system has been tested at Fedosiya to increase its rating to 2900 to 3200 kg for use on Voskhod-3. Three parachutes in these tests suffered rips during deployment. The Voskhod-3 capsule will weigh 3000 kg. Tkachev says he will guarantee its safety, but VVS and LII specialists do not share this optimism. Leonov, Gagarin, and various cosmonauts ask Kamanin to stop further showings of the new film comedy "30-3", which they say denigrates Soviet cosmonauts. However a showing to the leadership is enjoyed by all, and they see no grounds for surpressing it.
References: 376.
1966 February 2 - 02:02 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.186GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 118 km (73 mi). References: 2.
1966 February 2 - 10:04 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.50UG. -
Spica ultraviolet spectra Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 175 km (108 mi). References: 2.
1966 February 2 - 21:32 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 450 / Agena D SS-01B 1623. -
KH-4A 1029 Nation: USA. Payload: KH-4A s/n 1029 / Agena D 1623. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 182 km (113 mi). Apogee: 428 km (265 mi). Inclination: 75.00 deg. Period: 90.60 min. COSPAR: 1966-007A. USAF Sat Cat: 1968. Decay Date: 1966-02-27. KH-4A. Both panoramic cameras were operational throughout. References: 2, 6.
1966 February 2 - 23:15 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL307. -
LUX Solar AC5 Solar x-ray and ultraviolet mission Nation: Australia. Agency: WRE/RAE. Apogee: 216 km (134 mi). References: 2.
1966 February 3 - -
Luna 9 Landing on the Moon (first Moon Landing) Nation: USSR.
1966 February 3 - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena C030. -
USAF C030 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1966 February 3 - 07:41 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta C. LV Configuration: Thor Delta C 445/D36. -
ESSA 1 Nation: USA. Program: Tiros. Payload: Tiros OT3. Mass: 138 kg (304 lb). Class: Earth. Type: Weather. Spacecraft: Tiros. Agency: ESSA. Perigee: 684 km (425 mi). Apogee: 806 km (500 mi). Inclination: 97.80 deg. Period: 99.70 min. COSPAR: 1966-008A. USAF Sat Cat: 1982. Environmental Survey Satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 2, 6.
1966 February 3 - 11:11 GMT - Launch Site: Vandenberg. Launch Complex: 395-D. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-87. -
Winter Ice operational test Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1966 February 3 - 18:31 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.159UA. -
Spheres (UM) Aeronomy mission Nation: USA. Agency: NASA. Apogee: 131 km (81 mi). References: 2.
1966 February 4 - 01:54 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.143UA. -
Spheres (UM) Aeronomy mission Nation: USA. Agency: NASA. Apogee: 152 km (94 mi). References: 2.
1966 February 4 - 23:19 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure CE-16. -
ESRO C15 / 1 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 120 km (70 mi). References: 2.
1966 February 5 - Launch Site: Baikonur. Launch Complex: LC67/21. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36-O. LV Configuration: R-36O 8K69 U22502 No. 02L. -
OGCh No. 02L Nation: USSR. Mass: 1,700 kg (3,700 lb). Spacecraft: OGCh. Agency: RVSN. Apogee: 200 km (120 mi). COSPAR: U660205A. Second suborbital test of the FOBS system. References: 2, 279.
1966 February 9 - Launch Vehicle: Titan. Model: Titan 2. -
The Combined Systems Acceptance Test of Gemini launch vehicle (GLV) 9 was successfully conducted in the vertical test facility at Martin-Baltimore. Nation: USA. Flight: Gemini 9. The vehicle acceptance team convened February 14 and concluded its review on February 17 by accepting the vehicle. Deerection of GLV-9 was completed February 25, and the vehicle was formally accepted by the Air Force March 8. Stage I arrived at Cape Kennedy on March 9, stage II on March 10.
1966 February 9 - 19:45 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 428 / Agena D SS-01B 2703. -
OPS 1439 Nation: USA. Payload: Ferret 9 / Agena D 2703. Mass: 1,500 kg (3,300 lb). Class: Sigint. Spacecraft: Ferret. Agency: NRO/USAF. Perigee: 507 km (315 mi). Apogee: 511 km (317 mi). Inclination: 82.00 deg. Period: 94.70 min. COSPAR: 1966-009A. USAF Sat Cat: 1997. Decay Date: 1969-09-26. References: 2, 6.
1966 February 10 - Launch Vehicle: Titan. Model: Titan 2. -
Gemini launch vehicle 8 and spacecraft 8 were electrically mated; the Electrical Interface Integrated Validation and Joint Guidance and Control Test was completed February 14. Nation: USA. Flight: Gemini 8. After data from this test were reviewed (February 15), the Joint Combined Systems Test was run February 16.
1966 February 10 - -
State Commission Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3, Voskhod 4, Voskhod 5. The commission, chaired by Tyulin, with attendance by Mishin, Tsybin, Shabarov, Kerimov, and others considers manned flight plans for 1966. The 20-day dog flight of Voskhod s/n 5 is expected to launch on 22-23 February. Kamanin notes that although he is not against the flight, it has no interest to the military. Launch of Voskhod 3 is set for 20-23 March. Kamanin names his crews for the flight - Volynov/Shonin and Beregovoi/Shatalov as back-ups. Only Pravetskiy objects to these selections, pushing Katys for the prime crew. This settled, Mishin announces he still intends to pursue the artificial gravity experiment on the flights of Voskhod s/n 7 and/or 8. Kamanin informs Mishin that he has requested for more than a year that this experiment be moved to a Soyuz flight - there are 700 kg of new military scientific equipment that has to be flown aboard Voskhod, leaving little room for nothing else. It is decided that the flights of Voskhod s/n 5 and 6 will be run from Moscow rather than from the cosmodrome. The state commission will return to Moscow immediately after launch for this purpose. Four groups of staff will follow the flight on four-hour shifts. Tyulin, Keldysh, and Mishin want engineer and scientist cosmonauts to be trained for early Soyuz flights. Kamanin agrees, telling them he will submit suitable candidates. The meeting goes well, possibly since in the absence of Korolev the commission is stacked with military representatives - of 17 members, 9 are military.
References: 376.
1966 February 10 - 00:55 GMT - Launch Site: Wallops Island. Launch Complex: LA3A. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-4A. LV Configuration: Scout X-4A S141C. -
Reentry 4B Re-entry vehicle test Nation: USA. Agency: NASA. Apogee: 175 km (108 mi). References: 2.
1966 February 10 - 05:51 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.188GE. -
Auroral electrons 1 Aurora mission Nation: USA. Agency: NASA. Apogee: 178 km (110 mi). References: 2.
1966 February 10 - 07:09 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.187GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 117 km (72 mi). References: 2.
1966 February 10 - 07:48 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.148GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 114 km (70 mi). References: 2.
1966 February 10 - 08:52 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. -
Cosmos 107 Nation: USSR. Payload: Zenit-2 11F61 s/n 34. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: MOM. Perigee: 216 km (134 mi). Apogee: 313 km (194 mi). Inclination: 65.00 deg. Period: 89.70 min. COSPAR: 1966-010A. USAF Sat Cat: 1998. Duration: 8.00 days. Decay Date: 1966-02-18. Area survey photo reconnaissance satellite. References: 2, 6,93.
1966 February 10 - 09:48 GMT - Launch Site: Vandenberg. Launch Complex: 576A1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 305D. -
NTMP KX-38 / Pod 32 Reentry test / plume mission Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi). References: 2.
1966 February 10 - 18:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.145GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 122 km (75 mi). References: 2.
1966 February 10 - 18:41 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.149GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 114 km (70 mi). References: 2.
1966 February 11 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1387. -
Follow-on operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1966 February 11 - 01:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 460. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1966 February 11 - 13:04 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 86D. -
NTMP KX-51 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi). References: 2.
1966 February 11 - 18:00 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. -
Cosmos 108 Nation: USSR. Program: DS. Payload: DS-U1-G s/n 1. Mass: 355 kg (782 lb). Class: Earth. Type: Ionosphere. Spacecraft: DS-U1-G. Agency: MO SSSR. Perigee: 220 km (130 mi). Apogee: 850 km (520 mi). Inclination: 48.80 deg. Period: 95.30 min. COSPAR: 1966-011A. USAF Sat Cat: 2002. Completed Operations Date: 1966-02-26. Decay Date: 1966-11-21. Studied the relationship between variations in the upper atmosphere and solar activity. References: 2, 6, 99.
1966 February 14 - Launch Vehicle: N1. -
N1 redesign to increase payload to 95 tonnes Nation: USSR. Program: Lunar L3. Following Korolev's death, Mishin discovered that growth of the mass of the L3 payload had taken the low earth orbit payload requirement to 95 tonnes, beyond the 75 tonne lifting capability of the N1. To achieve the 95 tonne payload, changes in plans and redesign of the N1 would be necessary. The measures taken were: reduction of the orbital inclination for the initial earth orbit from 65 degrees to 52 degrees; reduce the altitude of the lunar orbit from 300 km to 220 km; increase the propellant mass by supercooling the propellants prior to loading in the lunach vehicle (the kerosene to be at -15 to -20 degrees Centigrade, the liquid oxygen to -191 degrees centigrade); add six engines to the first stage; increase thrust of all the engines on the first, second, and third stages by 2%; add a fourth stabilizer. The result of all of these measures would increase the launch mass to 2800 tonnes and the payload to the required 95 tonnes.
References: 21.
1966 February 15 - -
L1 trainers Nation: USSR. Program: Voskhod, Lunar L1. Spacecraft: Voskhod, Soyuz 7K-L1. Flight: Voskhod 3, Voskhod 4, Voskhod 5. Tyulin lays out the military experiments that are to be conducted aboard Voskhod during 1966. Plans for completion of an L1 trainer for preparations for a Soviet circumlunar flight are discussed. References: 376.
1966 February 15 - 20:30 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3 Agena D. LV Configuration: SLV-3 Agena D 7115 / Agena D 7115. -
KH 7-25 Nation: USA. Payload: KH-7 no. 25. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-7. Agency: NRO/USAF. Perigee: 142 km (88 mi). Apogee: 290 km (180 mi). Inclination: 96.50 deg. Period: 88.90 min. COSPAR: 1966-012A. USAF Sat Cat: 2012. Decay Date: 1966-02-22. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
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Bluebell 2C (Cylinder) Nation: USA. Payload: OPS 3011. Mass: 9.00 kg (19.80 lb). Class: Calibration. Spacecraft: Bluebell. Agency: USAF. Perigee: 115 km (71 mi). Apogee: 253 km (157 mi). Inclination: 96.50 deg. Period: 88.10 min. COSPAR: 1966-012B. USAF Sat Cat: 2014. Decay Date: 1966-02-16. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
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Bluebell 2S (Sphere) Nation: USA. Payload: OPS 3031. Mass: 4.00 kg (8.80 lb). Class: Calibration. Spacecraft: Bluebell. Agency: USAF. Perigee: 147 km (91 mi). Apogee: 268 km (166 mi). Inclination: 96.50 deg. Period: 88.60 min. COSPAR: 1966-012C. USAF Sat Cat: 2015. Decay Date: 1966-02-22. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
1966 February 16 - Launch Site: Vandenberg. Launch Complex: LF25. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2033. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1966 February 17 - Launch Vehicle: Titan. Model: Titan 2. -
The tanking test of Gemini launch vehicle (GLV) 8 was conducted. Nation: USA. Flight: Gemini 8. While the launch vehicle was being cleaned up after the test, spacecraft No. 8 Final Systems Test was completed February 23. On February 25, GLV and spacecraft were temporarily mated for an erector-cycling test. The extravehicular support package and life support system were checked out and installed in the spacecraft between February 26 and March 5, while GLV systems were modified and revalidated February 28 to March 3.
1966 February 17 - -
Soviet Lunar Landing Plans Nation: USSR. Program: Lunar L3. Spacecraft: Soyuz 7K-LOK, LK. Flight: Soviet Lunar Landing. Kamanin presents his plan to train 5 to 6 crews for the lunar landing mission over a 30 month period. Only experienced cosmonauts, with prior spaceflight experience, will be assigned to these crews. Kamanin lays out for the VVS leadership the complex series of events the cosmonauts will have to complete in the L3 lunar-orbit rendezvous scheme, including transfer between spacecraft of a single lunar landing cosmonaut in free space in lunar orbit. Crews need to be formed immediately, with two cosmonauts per crew - the L3 mission commander, and the second cosmonaut who will land on the moon. In order to accomplish the mission on schedule, a new air regiment needs to be formed, with the necessary flying laboratories, simulators and trainers, space suits, test stands and surface simulators, and other equipment necessary to train the crew for the mission.
References: 376.
1966 February 17 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-14. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 February 17 - Launch Site: Green River. Launch Complex: Pad 2. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena D014. -
USAF D014 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1966 February 17 - 08:33 GMT - Launch Site: Hammaguira. Launch Complex: Brigitte. Launch Pad: -. Launch Vehicle: Diamant. Model: Diamant A. LV Configuration: Diamant A No. 2. -
Diapason Nation: France. Payload: D-1A. Mass: 19 kg (41 lb). Class: Earth. Type: Geodetic. Spacecraft: D. Agency: CNES. Perigee: 502 km (311 mi). Apogee: 2,484 km (1,543 mi). Inclination: 34.10 deg. Period: 115.80 min. COSPAR: 1966-013A. USAF Sat Cat: 2016. Scientific satellite 'D-I' launched from Hammaguir (Algeria). References: 2, 6.
1966 February 17 - 09:45 GMT - Launch Site: Vandenberg. Launch Complex: 395-B. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-61. -
Black Hawk operational test Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1966 February 17 - 16:16 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.243UE. -
E / B currents Plasma mission Nation: USA. Agency: NASA. Apogee: 186 km (115 mi). References: 2.
1966 February 18 -
1966 February 18 - -
Cosmos 110 State Commission Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3. The first launch commission with Korolev's chair empty. The chief designers certify the full readiness of the booster, spacecraft, and the dogs that will crew the spacecraft. It is declared that the launch can proceed on 22-23 February. The only problem discussed is continued disquiet with the parachute system. Rips in the parachute have developed in the last four tests at Fedosiya. The system was designed for the original Vostok capsule mass of 2.6 tonnes, but the next Voskhods will have capsule landing weighs of 3.0 to 3.3 tonnes. Comrade Tkachev now refuses to guarantee the reliability of the system at landing weights over 2.9 to 3.0 tonnes. The Voronezhsk factory guarantees the reliability of the four third stage engines, despite the explosion of an engine on the test stand in December 1965. Launch of spacecraft s/n 6, Voskhod 3, is set for 22-23 March, with landing on 12 April. Afterwards the endless discussion of the role of IMBP in manned spaceflight, and especially military spaceflight is hashed over again in a bitter argument.
References: 376.
1966 February 18 - 04:56 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.189GE. -
Auroral electrons 2 Aurora mission Nation: USA. Agency: NASA. Apogee: 209 km (129 mi). References: 2.
1966 February 19 - 00:05 GMT - Launch Site: Arecibo. Launch Complex: VB. Launch Pad: -. Launch Vehicle: Javelin. Model: Nike Javelin. LV Configuration: Nike Javelin CRL AFS.502. -
REDLAMP ROBIN Ionosphere / aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 192 km (119 mi). References: 2.
1966 February 19 - 08:52 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 109 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: 288 km (178 mi). Inclination: 64.90 deg. Period: 89.40 min. COSPAR: 1966-014A. USAF Sat Cat: 2019. Duration: 8.00 days. Decay Date: 1966-02-27. High resolution photo reconnaissance satellite; returned film capsule; also carried biological experiments. References: 2, 6.
1966 February 19 - 09:56 GMT - Launch Site: Vandenberg. Launch Complex: 576B1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 73D. -
NTMP KX-47 Re-entry Vehicle test Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi). References: 2.
1966 February 20 - 00:10 GMT - Launch Site: Arecibo. Launch Complex: VB. Launch Pad: -. Launch Vehicle: Javelin. Model: Nike Javelin. LV Configuration: Nike Javelin CRL AFS.504. -
REDLAMP Ionosphere / aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 192 km (119 mi). References: 2.
1966 February 20 - 05:30 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.162UA. -
JHU Aurora 4 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 166 km (103 mi). References: 2.
1966 February 20 - 05:45 GMT - Launch Site: Arecibo. Launch Complex: VB. Launch Pad: -. Launch Vehicle: Javelin. Model: Nike Javelin. LV Configuration: Nike Javelin CRL AFS.505. -
REDLAMP TONI Ionosphere / aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 192 km (119 mi). References: 2.
1966 February 21 - Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. FAILURE: First stage failed 83 seconds after launch. -
DS-K-40 s/n 2 Nation: USSR. Program: DS. Payload: DS-K-40. Class: Technology. Spacecraft: DS-K-40. Agency: RVSN. COSPAR: F660221A. Development of systems for the later operational Tselina satellites. References: 2.
1966 February 21 - 13:10 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3. LV Configuration: Black Brant III NC7.181. -
Aeronomy mission Nation: USA. Agency: NRL. Apogee: 175 km (108 mi). References: 2.
1966 February 21 - 19:57 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3. LV Configuration: Black Brant III NC7.180. -
Aeronomy mission Nation: USA. Agency: NRL. Apogee: 188 km (116 mi). References: 2.
1966 February 21 - 20:23 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3. LV Configuration: Black Brant III NC7.178. -
O2 density Aeronomy mission Nation: USA. Agency: NRL. Apogee: 196 km (121 mi). References: 2.
1966 February 22 - -
Voskhod 3 flight authorised. Nation: USSR. Spacecraft: Voskhod. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On Performing in March 1966 the Launch 3KV n6 With Two Cosmonauts for Solving Problems of Extended Space Flight((8-20 Days)--course of Voskhod-3 preparations' was issued. References: 474.
1966 February 22 - 18:28 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure CE-13. -
ESRO C14 / 1 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 115 km (71 mi). References: 2.
1966 February 22 - 20:09 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. LV Configuration: Voskhod 11A57 R15000-06. -
Cosmos 110 Nation: USSR. Program: Voskhod. Payload: Voskhod 3KV s/n 5. Mass: 5,700 kg (12,500 lb). Class: Manned. Type: Spacecraft. Spacecraft: Voskhod. Agency: MOM. Perigee: 181 km (112 mi). Apogee: 887 km (551 mi). Inclination: 51.80 deg. Period: 95.30 min. COSPAR: 1966-015A. USAF Sat Cat: 2070. Duration: 20.69 days. Decay Date: 1966-03-16. Flight: Voskhod 3. Successfully recovered March 15, 1966 13:00 GMT. Precursor mission for Voskhod 3 hardware. Two dogs carried into lower Van Allen radiation belts. Officially: Biological research.Voskhod s/n 5 launched at 23:10 Moscow time, with two dogs, Veterka and Ygolka, aboard. This will be a 25-day mission. Kamanin is disgusted, he had proposed this as a 25-day mission by a single cosmonaut, but Korolev had constantly held with the 'dog variant'. Preparations for Voskhod-3 are proceeding well. The prime and back-up crews have completed their training and will take their examinations on 28 February. Parallel trials of the oxygen regeneration system at IMBP and OKB-124 both went well (IMBP, 12 days so far, temperature 16-24 deg C, 70% humidity; OKB-124, 10 days so far, temperature 18-16 deg C, 65% humidity).
References: 2, 6, 376.
1966 February 23 - 10:06 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 186. -
Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi). References: 2.
1966 February 23 - 23:14 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure CE-14. -
ESRO C14 / 2 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 117 km (72 mi). References: 2.
1966 February 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-380. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 February 24 - 19:40 GMT - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 629 (63-112). -
Follow-on operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1966 February 24 - 19:40 GMT - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 529 (63-005). -
Follow-on operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1966 February 25 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 February 25 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 February 25 - 13:59 GMT - Launch Site: Sonmiani. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.211IA. -
Rehbar 9 (Na) Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1966 February 26 - Launch Site: Kapustin Yar. Launch Complex: PL87. Launch Pad: -. Launch Vehicle: RT-2. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1966 February 26 - 13:59 GMT - Launch Site: Sonmiani. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.212IA. -
Rehbar 10 (Na) Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1966 February 26 - 16:12 GMT - Launch Site: Cape Canaveral. Launch Complex: LC34. Launch Pad: -. Launch Vehicle: Saturn I. Model: Saturn IB. LV Configuration: Saturn IB SA-201. -
Apollo 201 (AS-201) Nation: USA. Agency: NASA. Apogee: 488 km (303 mi). Apollo-Saturn 201 was launched from Cape Kennedy, with liftoff of an Apollo Block I spacecraft (CSM 009) on a Saturn IB launch vehicle at 11:12:01 EST. Launched from Launch Complex 34, the unmanned suborbital mission was the first flight test of the Saturn IB and an Apollo spacecraft. Total launch weight was 22,000 kilograms.Spacecraft communications blackout lasted 1 minute 22 seconds. Reentry was initiated with a space-fixed velocity of 29,000 kilometers per hour. CM structure and heatshields performed adequately. The CM was recovered by the USS Boxer from the Atlantic about 72 kilometers uprange from the planned landing point. (8.18 S x 11.15 W).
References: 2.
1966 February 27 - 16:51 GMT - Launch Site: Ascension. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.251UM. -
UM Pitot 20 / AS-201 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 155 km (96 mi). References: 2.
1966 February 28 - -
Gemini IX Astronauts Elliot M. See, Jr., and Charles A. Bassett II killed when their T-38 jet crashed. Nation: USA. Flight: Gemini 9, Gemini 9A. Gemini IX Astronauts Elliot M. See, Jr., and Charles A. Bassett II were killed when their T-38 jet training plane crashed in rain and fog short of the St. Louis Municipal Airport. The jet, which had been cleared for an instrument landing, was left of center in its approach to the runway when it turned toward the McDonnell complex, 1000 feet from the landing strip. It hit the roof of the building where spacecraft nos. 9 and 10 were being housed, bounced into an adjacent courtyard, and exploded. Several McDonnell employees were slightly injured. Minutes later the Gemini IX backup crew, Thomas P. Stafford and Eugene A. Cernan, landed safely. The four astronauts were en route to McDonnell for two weeks' training in the simulator. NASA Headquarters announced that Stafford and Cernan would fly the Gemini IX mission on schedule and appointed Alan B. Shepard, Jr., to head a seven-man investigating team.
1966 February 28 - Launch Vehicle: Titan. Model: Titan 2. -
Stage I of Gemini launch vehicle 10 was erected in the east cell of the vertical test facility at Martin-Baltimore. Nation: USA. Flight: Gemini 10. After completing horizontal testing March 3, stage II was erected March 7. Power was applied to the vehicle for the first time on March 14. Subsystems Functional Verification Tests were completed April 13.
1966 February 28 - -
Astronaut Elliott McKay See Jr dies at age of 38 -- Crash of T-38 trainer into the McDonnell Aircraft plant. Nation: USA.
1966 February 28 - 13:58 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta E. LV Configuration: Thor Delta E 461/D37. -
ESSA 2 Nation: USA. Program: Tiros. Payload: Tiros OT2. Mass: 132 kg (291 lb). Class: Earth. Type: Weather. Spacecraft: Tiros. Agency: ESSA. Perigee: 1,355 km (841 mi). Apogee: 1,415 km (879 mi). Inclination: 101.30 deg. Period: 113.50 min. COSPAR: 1966-016A. USAF Sat Cat: 2091. Environmental Survey Satellite; carried APT cameras. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 2, 6.
1966 March 1 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. -
Vandenberg, adds 14,890 acres Nation: USA. Vandenberg, adding approximately 14,890 acres to the base and increasing its size to its present 98,400 acres. References: 88.
1966 March 1 - -
Venera 3, Venus Impact (USSR) Nation: USSR.
1966 March 1 - -
Voskhod 3 postponed Nation: USSR. Program: Voskhod. Flight: Voskhod 3. Tyulin advises that the State Commission has decided to postpone the flight of Voskhod 3 to late April. The cosmonauts ready, but the spacecraft is not. OKB-1 staff at Baikonur also are tasked to launch the Luna 10 probe and another Molniya-1 communications satellite before Voskhod 3 can be launched. No fixed date for the manned launch has been set.
References: 376.
1966 March 1 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 March 1 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 March - -
Venera x impacts on Venus Nation: USSR. Spacecraft: Venera 3MV-3. The mission of this spacecraft 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 but, the communications systems failed before planetary data could be returned.
1966 March 1 - 11:03 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M N103-41. FAILURE: The escape stage Block L lost roll control during unpowered coast in parking orbit because the axis of the course regulator of the control system jammed in the zero position. The stage's engine was not fired. -
Cosmos 111 Nation: USSR. Program: Luna. Payload: Ye-6S s/n 204. Mass: 6,540 kg (14,410 lb). Class: Planetary. Type: Lunar. Spacecraft: Luna E-6S. Agency: NII-88. Perigee: 168 km (104 mi). Apogee: 180 km (110 mi). Inclination: 51.80 deg. Period: 88.00 min. COSPAR: 1966-017A. USAF Sat Cat: 2093. Decay Date: 1966-03-03. References: 2, 6, 64, 65.
1966 March 2 - 17:55 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.99DS. -
Te, Solar UV Solar extreme ultraviolet mission Nation: USA. Agency: NASA. Apogee: 228 km (141 mi). References: 2.
1966 March 2 - 17:59 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.25GA-GI. -
Geoprobe Aeronomy / ionosphere mission Nation: USA. Agency: NASA. Apogee: 536 km (333 mi). References: 2.
1966 March 3 - -
Landing rocket system for Apollo. Nation: USA. Spacecraft: Apollo CSM, Apollo X. Associate Administrator for Manned Space Flight George E. Mueller acknowledged receipt from Joseph F. Shea, the Apollo Spacecraft Program Manager at MSC, of a detailed technical description of MSC's plans and development progress toward developing a landing rocket system for Apollo. (MSC had undertaken this effort some months earlier at Mueller's specific request.) Mueller advised Shea that he had asked AAP Deputy Director John H. Disher to work closely with Shea's people to devise a land landing system for AAP built on Houston's effort for Apollo.
1966 March 3 - -
Voskhod 3 ECS Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3. Today the trials at Voronin's OKB-124 had to be halted after a 16 day run, when the cabin oxygen level went out of limits. It seems the cosmonauts could control it in flight by closely monitoring the cabin atmosphere composition and changing cartridges as necessary (typically after 5.5 days), but this is not a reliable basis for a flight. For a 20 day flight, a 22-day endurance run on earth should be a minimum, but neither the IMBP or OKB-124 have been able to make the system run longer than 14-16 days before it breaks down. Later the State Commission meets. Cosmos 110 continues in normal flight, the dogs and other life forms are alive. The only minus is that data received is complete due to the failure of the antennae to deploy.
References: 376.
1966 March 3 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-135. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 March 3 - 21:54 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.100DS. -
AFCRL Solar Solar extreme ultraviolet mission Nation: USA. Agency: NASA. Apogee: 219 km (136 mi). References: 2.
1966 March 3 - 22:26 GMT - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C77. -
Solar ultraviolet mission Nation: France. Agency: CNES. Apogee: 125 km (77 mi). References: 2.
1966 March 4 - 12:29 GMT - Launch Site: Vandenberg. Launch Complex: 576A1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 303D. FAILURE: Failure. -
NTMP KX-35 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi). References: 2.
1966 March 5 - 04:50 GMT - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: -. Launch Vehicle: Lambda. Model: Lambda 3H. LV Configuration: Lambda 3H L-3H-1. -
X-ray astronomy mission Nation: Japan. Agency: ISAS. Apogee: 1,829 km (1,136 mi). References: 2.
1966 March 6 - Launch Vehicle: N1, R-9, RT-2. -
Soviet design bureaux reorganised and renamed. Nation: USSR. Spacecraft: LK, Soyuz 7K-LOK, Soyuz 7K-OK, Soyuz 7K-L1. Decree 'On renaming OKB-1 as TsKBEM and OKB-52 as TsKBM' was issued. In 1966 Afanasyev reorganised the military industrial complex. OKB-1 was redesignated TsKBEM. Sergei Osipovich Opakhin was made First Deputy within the new organization.However within TsKBEM there were no relative priorities for the projects competing for resources. The R-9 and RT-2 ICBM's, the orbital, circumlunar, and lunar orbiter versions of Soyuz, the LK lunar lander, the N1 booster -- all were 'equal'. It seemed folly to be pursuing the orbital ferry version of the Soyuz when no space station had to be funded. But it was felt flying the spacecraft would solve reliability questions about the design, so it was pursued in parallel with the L1 and L3 versions.
References: 367, 474.
1966 March 8 - -
Dual Apollo AS-207/208 mission planned Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Apollo Program Director Samuel C. Phillips notified the three manned space flight Centers that they were requested to plan for a dual AS-207/208 mission, assuming that launch would occur one month later than the 207 launch now scheduled. References: 16.
1966 March 8 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1362. -
Follow-on operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1966 March 8 - 07:42 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.148CG. -
AS / E with ACS X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 165 km (102 mi). References: 2.
1966 March 9 - -
Douglas proposal on the airlock for the AAP. Nation: USA. Spacecraft: Orbital Workshop. A team of engineers from Douglas Aircraft Company, headed by Jack Bromberg, presented a technical briefing and cost proposal to Associate Administrator for Manned Space Flight George E. Mueller on the company's design on the airlock for the AAP. Mueller observed that Douglas' idea for a 30-day capability seemed technically sound. He expressed strong interest in the AAP spent-stage experiment because it would establish a solid basis for space station requirements and definition. However, he cautioned that he had not received definite approval from either the Administrator, James E. Webb, or his deputy, Robert C. Seamans, Jr., on the spent-stage concept and admitted that he had 'some selling to do.'
1966 March 9-10 - -
First integrated test of major Apollo service module systems Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The first integrated test of the service propulsion system, electrical power system, and cryogenic gas storage system was successfully conducted at the White Sands Test Facility. References: 16.
1966 March 9 - 02:22 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 KP3.15. -
Stellar spectra Ultraviolet astronomy mission Nation: USA. Agency: KPNO. Apogee: 150 km (90 mi). References: 2.
1966 March 9 - 22:02 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 452 / Agena D SS-01B 1622. -
KH-4A 1030 Nation: USA. Payload: KH-4A s/n 1030 / Agena D 1622. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 180 km (110 mi). Apogee: 418 km (259 mi). Inclination: 75.00 deg. Period: 90.40 min. COSPAR: 1966-018A. USAF Sat Cat: 2099. Decay Date: 1966-03-29. KH-4A. All cameras operated satisfactorily. References: 2, 6.
1966 March 10 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-383. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 March 10 - Launch Site: White Sands. Launch Complex: LC33. Launch Pad: -. Launch Vehicle: Javelin. Model: Nike Javelin. -
DASA HAR Aeronomy mission Nation: USA. Agency: DASA?. Apogee: 200 km (120 mi). References: 2.
1966 March 10 - 08:45 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AF07.327. -
Bremss density Ionosphere mission Nation: USA. Agency: AFCRL. Apogee: 205 km (127 mi). References: 2.
1966 March 10 - 22:25 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure CE-11. -
ESRO C13 / 2 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 114 km (70 mi). References: 2.
1966 March 11 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1211. -
Follow-on operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1966 March 12 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3C. -
Start of construction (site preparation) for SLC-6 Nation: USA. Class: Manned. Type: Space station. Spacecraft: MOL. Start of construction (site preparation) for Space Launch Complex 6 facilities at former Sudden Ranch property. References: 88.
1966 March 12 - -
Voskhod/Soyuz crews Nation: USSR. Program: Voskhod. Flight: Voskhod 4, Voskhod 5, Soyuz 1, Soyuz 2A. Tyulin and Mozzhorin review with Kamanin crewing plans. Even though the missions of Voskhod 4 and 5 are not yet clear, Tyulin wants to settle on Beregovoi and Katys for Voskhod 4, and Ponomaryova and Solovyova for Voskhod 5. Since October 1965 six crews have been in training for Soyuz flights: Gagarin -Voronov, Nikolayev-Gorbatko, Bykovsky-Matinchenko, Komarov-Kolodin, Zaikin-Khrunov, and Popovich-Artyukhin. But these are just nominal groupings, and firm crew assignments by mission have not yet been made.
References: 376.
1966 March 12 - 00:42 GMT - Launch Site: Johnston Island. Launch Complex: LE2. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2J. LV Configuration: Thor DSV-2J 196. -
AFP-437(AP) interceptor mission Nation: USA. Agency: USAF. Apogee: 472 km (293 mi). References: 2.
1966 March 13 - Launch Site: Hammaguira. Launch Complex: Brigitte. Launch Pad: -. Launch Vehicle: Diamant. Model: Saphir. LV Configuration: Saphir VE231 G1. -
Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 1,000 km (600 mi). References: 2.
1966 March 13 - 05:13 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.190GE. -
Auroral electrons 3 Aurora mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1966 March 14 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 March 14 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 March 14 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 March 14 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1966 March 15 - -
Cosmos 110 landing commission Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3. The State Commission meets on the 21st day of flight. The life forms are still alive, although the atmosphere in the cabin isgradually worsening (oxygen has gone from 143 to 136 mm Hg and the carbon dioxide level has gone up from 0.89% to 0.91%). The flight duration objective has been fulfilled, and although the designers say the ECS could run for a total of 36 days, it is decided to bring the capsule down within the next two days. A landing commission of 25 military and engineering representatives is formed to oversee the process. It is decided to bring the capsule down on the 330th orbit, on 16 March, with an emergency re-entry possible at 15:30 on 15 March if the cabin parameters worsen.
References: 376.
1966 March 16 - -
Landing of Cosmos 110 Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3. The 'Spusk' landing command is transmitted to the capsule at 14:00,
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