1967 July 1 - Launch Vehicle: Tsiklon. Model: Tsyklon 2. -
Tsiklon-2 launch vehicle authorised. Nation: USSR. Spacecraft: US-A, IS-A, Meteor. Council of Soviet Ministers (SM) Decree 'On use of the R-36-based launcher for the Kosmos and Meteor satellites' was issued. References: 474.
1967 Q3? - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. -
Test launch Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1967 Q3? - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. -
Test launch Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1967 July 1 - 13:15 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3C. LV Configuration: Titan IIIC 3C-14. -
IDCSP 3-1 Nation: USA. Payload: IDCSP 16. Mass: 45 kg (99 lb). Class: Communications. Type: Military. Spacecraft: IDCSP. Agency: USAF. Perigee: 33,030 km (20,520 mi). Apogee: 33,515 km (20,825 mi). Inclination: 11.90 deg. Period: 1,309.60 min. COSPAR: 1967-066A. USAF Sat Cat: 2862. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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IDCSP 3-2 Nation: USA. Payload: IDCSP 17. Mass: 45 kg (99 lb). Class: Communications. Type: Military. Spacecraft: IDCSP. Agency: USAF. Perigee: 33,046 km (20,533 mi). Apogee: 33,517 km (20,826 mi). Inclination: 11.90 deg. Period: 1,310.00 min. COSPAR: 1967-066B. USAF Sat Cat: 2863. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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IDCSP 3-3 Nation: USA. Payload: IDCSP 18. Mass: 45 kg (99 lb). Class: Communications. Type: Military. Spacecraft: IDCSP. Agency: USAF. Perigee: 33,079 km (20,554 mi). Apogee: 33,547 km (20,845 mi). Inclination: 11.90 deg. Period: 1,311.60 min. COSPAR: 1967-066C. USAF Sat Cat: 2864. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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IDCSP 3-4 Nation: USA. Payload: IDCSP 19/DATS. Mass: 68 kg (149 lb). Class: Communications. Type: Military. Spacecraft: IDCSP. Agency: USAF. Perigee: 33,145 km (20,595 mi). Apogee: 33,560 km (20,850 mi). Inclination: 11.90 deg. Period: 1,313.50 min. COSPAR: 1967-066D. USAF Sat Cat: 2865. Antenna tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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LES 5 Nation: USA. Mass: 194 kg (427 lb). Class: Technology. Type: Comsat. Spacecraft: LES. Agency: USAF. Perigee: 33,196 km (20,626 mi). Apogee: 33,609 km (20,883 mi). Inclination: 12.00 deg. Period: 1,316.00 min. COSPAR: 1967-066E. USAF Sat Cat: 2866. Experimental commsat. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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DODGE 1 Nation: USA. Mass: 102 kg (224 lb). Class: Technology. Type: Gravity gradient. Spacecraft: DODGE. Agency: USN NASC. Perigee: 33,257 km (20,664 mi). Apogee: 33,670 km (20,920 mi). Inclination: 12.00 deg. Period: 1,319.10 min. COSPAR: 1967-066F. USAF Sat Cat: 2867. Gravity gradient experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1967 July 4 - 05:59 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. LV Configuration: Voskhod 11A57 Ya15001-05. -
Cosmos 168 Nation: USSR. Payload: Zenit-2 11F61 s/n 52. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: MOM. Perigee: 223 km (138 mi). Apogee: 230 km (140 mi). Inclination: 51.80 deg. Period: 89.10 min. COSPAR: 1967-067A. USAF Sat Cat: 2869. Duration: 8.00 days. Decay Date: 1967-07-12. Area survey photo reconnaissance satellite. References: 2, 6,93.
1967 July 5 - -
Fire that at White Sands Apollo Test Stand 403 Nation: USA. Program: Apollo. Spacecraft: Apollo LM. A board was appointed by MSC White Sands Test Facility Manager Martin L. Raines to determine the cause of a fire that had occurred at Test Stand 403 on July 3. The board was to submit its findings by July 17. References: 16.
1967 July 5 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1126. -
FOT GB40 Follow-on Test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1967 July 5 - 14:07 GMT - Launch Site: Biscarosse. Launch Complex: -. Launch Pad: -. Launch Vehicle: Diamant. Model: Rubis. LV Configuration: Rubis R10. -
Rubis 04 Astronomy mission Nation: France. Agency: CNES. Apogee: 1,560 km (960 mi). Radio-astronomy experiment; measured the MHz range radio background References: 2.
1967 July 5 - 18:41 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 CRL AE3.582. -
Auroral profile Aurora mission Nation: USA. Agency: AFCRL. Apogee: 200 km (120 mi). References: 2.
1967 July 6 - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 65D. -
ABRES PDV re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi). References: 2.
1967 July 8 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P. -
Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1967 July 8 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P. -
Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1967 July 8 - 04:10 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.190UG. -
MIT X-ray X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 142 km (88 mi). References: 2.
1967 July 11 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Combat training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1967 July 12 - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 800. -
FOT GB42 Follow-on Test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1967 July 13 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 779. -
ST Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1967 July 14 - Launch Site: Green River. Launch Complex: Pad 2. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena D050. -
USAF D050 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1967 July 14 - 11:53 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36A. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Centaur D. LV Configuration: Atlas Centaur D AC-11 / Centaur D 291D. -
Surveyor 4 Nation: USA. Payload: Surveyor SC-4. Mass: 283 kg (623 lb). Class: Planetary. Type: Lunar. Spacecraft: Surveyor. Agency: NASA/JPL. COSPAR: 1967-068A. USAF Sat Cat: 2875. Decay Date: 1967-07-17. Soft lunar landing attempt failed. References: 2, 6, 278.
1967 July 15 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 755. -
GIN BABY I research and development mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1967 July 15 - Launch Site: Vandenberg. Launch Complex: LF21. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2337. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1967 July 15 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. FAILURE: Failure. -
Combat training launch Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1967 July 16 -
1967 July 17 - 16:45 GMT - Launch Site: Baikonur. Launch Complex: LC162/36. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36-O. LV Configuration: R-36O 8K69 Ya22500 No. 11L. -
Cosmos 169 Nation: USSR. Mass: 1,700 kg (3,700 lb). Class: Military. Type: FOBS. Spacecraft: OGCh. Agency: RVSN. Perigee: 135 km (83 mi). Apogee: 200 km (120 mi). Inclination: 49.70 deg. Period: 87.80 min. COSPAR: 1967-069A. USAF Sat Cat: 2878. Decay Date: 1967-07-17. Fractional Orbital Bombardment system test. References: 2, 6.
1967 July 19 - 14:19 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta E1. LV Configuration: Thor Delta E1 488/D50. -
Explorer 35 Nation: USA. Program: Explorer. Payload: AIMP E. Mass: 104 kg (229 lb). Class: Earth. Type: Magnetosphere. Spacecraft: IMP. Agency: NASA GSF. Perigee: 484 km (300 mi). Apogee: 675 km (419 mi). Inclination: 32.40 deg. Period: 96.26 min. COSPAR: 1967-070A. USAF Sat Cat: 2884. Earth magnetic tail measurements. Lunar Orbit (Selenocentric). The Westinghouse Aerospace Division, under contract to National Aeronautics and Space Administration's Goddard Space Flight Center, engaged in the system design, integration, assembly and launch support for Anchored Interplanetary Monitoring Platform Satellite, officially designated Explorer 35 by the National Aeronautics and Space Administration. It was launched on July 19, 1967, with the primary objectives of investigation of interplanetary plasma and the interplanetary magnetic field out to and at the lunar distance, in either a captured lunar orbit or a geocentric orbit of the earth. In the geocentric orbit, the apogee was near or beyond the lunar distance. In a lunar orbit, additional objectives included obtaining data on dust distribution, lunar gravitational field, ionosphere, magnetic field, and radiation environment around the moon. AIMP-E also studied spatial and temporal relationships of geophysical and interplanetary phenomena simultaneously being studied by several other National Aeronautics and Space Administration satellites. The investigation in the vicinity of the moon provided for measurements of the characteristics of the interplanetary dust distribution, solar and galactic cosmic rays, as well as a study of the magnetohydrodynamic wake of the earth in the interplanetary medium at the lunar distances.
References: 2, 6, 405.
1967 July 20 - Launch Site: Baikonur. Launch Complex: PU32. Launch Pad: PU32?. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
SBP Special test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1967 July 20 - Launch Site: Vandenberg. Launch Complex: LF22. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2370. -
ST Olympic Trials 3 operational test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1967 July 20 - 09:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.212UA. -
Composition Aeronomy mission Nation: USA. Agency: NASA. Apogee: 210 km (130 mi). References: 2.
1967 July 20 - 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 3-61-91. -
X-15A HT/Guid/Telem test Nation: USA. Agency: NASA/USAF. Apogee: 25 km (15 mi). Maximum Speed - 5942 kph. Maximum Altitude - 25720 m. References: 2.
1967 July 20 - 19:24 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.211UA. -
Composition Aeronomy mission Nation: USA. Agency: NASA. Apogee: 209 km (129 mi). References: 2.
1967 July 21 - Launch Vehicle: Soyuz, Tsiklon. -
US Project reassigned; R-36-O booster development approved; Yantar-2K and Zvevda 7K-VI approved. Nation: USSR. Spacecraft: US-A, US-P, Yantar-2K, Yantar-4K1, Soyuz VI. Decree 715-240 'On the Creation of Space Systems for Naval Reconnaissance Comprising the US sat and the R-36-based booster -further work on the US naval reconnaissance satellite, approval of work on the Yantar-2K, and course of work on 7K-VI Zvezda'.An entire family of Yantar spacecraft was proposed by Kozlov’s design bureau during the initial development; information on two film return models has been declassified. Yantar was initially derived from the Soyuz spacecraft, including systems developed for the Soyuz VI military model. During design and development this changed until it had very little in common with Soyuz. Following numerous problems in the first flight tests of the Soyuz 7K-OK, Kozlov ordered a complete redesign of the 7K-VI manned military spacecraft. The new spacecraft, with a crew of two, would have a total mass of 6.6 tonnes and could operate for a month in orbit. The new design switched the positions of the Soyuz descent module and the orbital modules and was 300 kg too heavy for the standard 11A511 launch vehicle. Therefore Kozlov designed a new variant of the Soyuz launch vehicle, the 11A511M. The project was approved by the Central Committee of the Communist Party, with first flight to be in 1968 and operations to begin in 1969. The booster design, with unknown changes to the basic Soyuz, did not go into full production.
References: 474.
1967 July 21 - Launch Vehicle: Tsiklon. -
R-36 ICBM accepted into service. Nation: USSR. Decree 'On approval of the R-36 ICBM variant with countermeasures to overcome anti-ballistic missiles and on adoption of the R-36 ICBM into armaments' was issued. References: 474.
1967 July 21 - Launch Vehicle: UR-700. -
Chelomei signs design documents for UR-700/LK-700 lunar expedition Nation: USSR. Spacecraft: LK-700. Chelomei's TsKBM began work on the UR-700 launch vehicle for manned lunar landing missions in 1962. Chelomei took a sound conservative design approach (i.e. no docking required, no cryogenics).
1967 July 21 - -
Soyuz spacecraft programme review is conducted. Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Problems are identified with the parachutes and oxygen regeneration system which must be solved before the first manned flight. References: 376.
1967 July 21 - 06:00 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. LV Configuration: Voskhod 11A57 Ya15001-14. FAILURE: Failure. -
Zenit-4 Nation: USSR. Spacecraft: Zenit-4. Agency: RVSN. COSPAR: F670721A. High resolution photo reconnaissance mission. References: 279.
1967 July 22 - Launch Site: Vandenberg. Launch Complex: 576A3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F/Trident. LV Configuration: Atlas F/Trident 114F. -
RMP-B-2 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi). References: 2.
1967 July 23 - 00:53 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.337CM. -
Vapor trail Aeronomy mission Nation: USA. Agency: NASA. Apogee: 204 km (126 mi). References: 2.
1967 July 24 - -
Yantar-2K reconnaissance satellite authorised. Nation: USSR. Spacecraft: Yantar-2K. Ministry of General Machine Building (MOM) Decree 220 'On approval of work on the Yantar-2K' was issued. References: 474.
1967 July 24 - -
Cosmonaut group meeting. Nation: USSR. Program: Lunar L1. Spacecraft: Soyuz 7K-L1. Mishin is seen as jeopardising Soviet manned lunar plans. He has no understanding of the necessity of providing proper training simulators to prepare the cosmonauts for flight. He is coarse, rude, doesn't listen to critics, and ignores the comments of those who will have to fly aboard his spacecraft. The cosmonauts agree they should request a meeting with Brezhnev and tell him flat out - there will be no moon landing as long as Mishin is in charge.
Additional Details: Cosmonaut group meeting. . References: 376.
1967 July 25 - -
Apollo lunar mapping and survey system terminated Nation: USA. Program: Apollo. Spacecraft: Apollo LMSS. Following a series of discussions on the requirements for the lunar mapping and survey system (LMSS), the effort was terminated. An immediate stop work order was issued to the Air Force, the Centers, and the contractors in the LMSS effort. The original justification for the LMSS, a backup Apollo site certification capability in the event of Surveyor or Lunar Orbiter inadequacies, was no longer valid, since at least four Apollo sites had been certified and the last Lunar Orbiter would, if successful, increase that to eight.
References: 16.
1967 July 25 - -
Apollo LM-2 options Nation: USA. Program: Apollo. Spacecraft: Apollo LM. MSC Director of Flight Operations Christopher C. Kraft, Jr., raised questions about lunar module number 2: Would it be possible for LM-2 to be a combined manned and unmanned vehicle; that is, have the capability to make an unmanned burn first and then be manned for additional activities? Would additional batteries in the LM provide greater flexibility for earth-orbital missions? Mission flexibility would be worthwhile only if it allowed deletion of a subsequent mission, at least on paper.
References: 16.
1967 July 25 - Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7A. -
Operational test Nation: USSR. Agency: RVSN. Apogee: 1,350 km (830 mi). References: 2.
1967 July 25 - 03:48 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 496 / Agena D SS-01B 2732. -
OPS 1879 Nation: USA. Payload: Ferret 11 / Agena D 2732. Mass: 1,500 kg (3,300 lb). Class: Sigint. Spacecraft: Ferret. Agency: NRO/USAF. Perigee: 390 km (240 mi). Apogee: 608 km (377 mi). Inclination: 75.10 deg. Period: 94.50 min. COSPAR: 1967-071A. USAF Sat Cat: 2890. Decay Date: 1969-06-05. References: 2, 6.
1967 July 26 -
1967 July 27 - Launch Site: Sary Shagan. Launch Complex: -. Launch Pad: -. Launch Vehicle: S-225. FAILURE: Failure. -
Dummy test Nation: USSR. Agency: PRO. Apogee: 0 km ( mi). References: 2.
1967 July 27 - 19:00 GMT - Launch Site: Vandenberg. Launch Complex: 576B3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 92D. FAILURE: Partial Failure. -
OV1-08S Nation: USA. Mass: 118 kg (260 lb). Class: Earth. Type: Magnetosphere. Spacecraft: OV1. Agency: USAF OAR. Perigee: 529 km (328 mi). Apogee: 557 km (346 mi). Inclination: 101.60 deg. Period: 95.50 min. COSPAR: 1967-072A. USAF Sat Cat: 2893. Decay Date: 1972-02-22. Carried cosmic ray telescope. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
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OV1-12S Nation: USA. Mass: 140 kg (300 lb). Class: Earth. Type: Magnetosphere. Spacecraft: OV1. Agency: USAF OAR. Perigee: 497 km (308 mi). Apogee: 579 km (359 mi). Inclination: 101.70 deg. Period: 95.40 min. COSPAR: 1967-072D. USAF Sat Cat: 2901. Decay Date: 1980-07-22. Solar flare observations. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
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OV1-11 Nation: USA. Spacecraft: OV1. Agency: USAF AFSC. COSPAR: 1967-072xx. USAF Sat Cat: 2893. Decay Date: 1972-02-22. OV-1 11 did not reach orbit. References: 2, 279.
1967 July 28 - 14:21 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 478 (TA8) / Agena D SS-01B 680. -
OGO 4 Nation: USA. Payload: OGO D (NASA S-50A). Mass: 634 kg (1,397 lb). Class: Earth. Type: Magnetosphere. Spacecraft: OGO. Agency: NASA GSF. Perigee: 422 km (262 mi). Apogee: 885 km (549 mi). Inclination: 86.00 deg. Period: 97.80 min. COSPAR: 1967-073A. USAF Sat Cat: 2895. Decay Date: 1972-08-16. OGO 4 was a large observatory instrumented with experiments designed to study the interrelationships between the aurora and airglow emissions, energetic particle activity, geomagnetic field variation, ionospheric ionization and recombination, and atmospheric heating which take place during a period of increased solar activity. After the spacecraft achieved orbit and the experiments were deployed into an operating mode, an attitude control problem occurred. This condition was corrected by ground control procedures until complete failure of the tape recording systems in mid-January 1969. At that time, due to the difficulty of maintaining attitude control without the tape recorders, the attitude control system was commanded off, and the spacecraft was placed into a spin-stabilized mode about the axis which was previously maintained vertically. In this mode, seven of the remaining experiments were turned off since no meaningful data could be observed by them. On October 23, 1969, the satellite was turned off. It was reactivated again in January 1970 for 2 months to obtain VLF observations.
References: 2, 6.
1967 July 29 -
1967 July 29 - 08:48 GMT - Launch Site: Vandenberg. Launch Complex: 576A2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 150F. -
ABRES MBRV-3 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi). References: 2.
1967 July 31 - -
Meeting of space programme management in the Crimea. Nation: USSR. Program: Almaz. Spacecraft: Soyuz OB-VI, Almaz OPS. Two planning documents are discussed. The first deals with the training of civilian cosmonauts. Two phases of training are planned, the first phase at MOM institutes and Minzorar, the second at TsPK and the VVS. In addition 50 new air force pilots will be identified for space duty in three groups in 1968, 1969, and 1970. They will be ready for the planned large number of 7K-VI and Almaz flights beginning in 1972. Brezhnev would like to see more Voskhod flights. Meanwhile Titov has qualified as a test pilot third class, and will qualify as second class by the end of the year. All in all, things are looking good in the years ahead.
References: 376.
1967 July 31 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-529. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1967 July 31 - 00:31 GMT - Launch Site: Kiruna. Launch Complex: C. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure 2B. LV Configuration: Centaure 2B CE-30. -
ESRO C20 / 1 Aeronomy mission Nation: Europe. Agency: ESRO. Apogee: 127 km (78 mi). References: 2.
1967 July 31 - 00:58 GMT - Launch Site: Kiruna. Launch Complex: C. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure 2B. LV Configuration: Centaure 2B CE-31. -
ESRO C32 / 1 Meteorite mission Nation: Europe. Agency: ESRO. Apogee: 130 km (80 mi). References: 2.
1967 July 31 - 16:45 GMT - Launch Site: Baikonur. Launch Complex: LC161/35. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36-O. LV Configuration: R-36O 8K69 Ya22500 No. 12L. -
Cosmos 170 Nation: USSR. Mass: 1,700 kg (3,700 lb). Class: Military. Type: FOBS. Spacecraft: OGCh. Agency: RVSN. Perigee: 141 km (87 mi). Apogee: 199 km (123 mi). Inclination: 49.60 deg. Period: 87.90 min. COSPAR: 1967-074A. USAF Sat Cat: 2902. Decay Date: 1967-07-31. Fractional Orbital Bombardment system test. References: 2, 6.
1967 August 1 - Launch Vehicle: Saturn I. Model: Saturn IB. -
AS-208 Nation: USA. Program: Apollo. Payload: LM-2. Class: Manned. Type: Lunar lander. Spacecraft: Apollo LM. Before fire, planned in-orbit test of LM. CSM-101 would dock with and crew would maneuver together. References: 26, 27.
1967 August 1 - -
NASA program to develop the technology of flexible wings for spacecraft recovery. Nation: USA. NASA's Office of Manned Space Flight and Office of Advanced Research and Technology were engaged in a cooperative program to develop the technology of flexible wings for spacecraft recovery. The technology was expected to have broad applicability in the Apollo Applications Program, as well as follow-on manned space flight programs. The principal technology effort would concentrate on parawing and sailwing configurations. LaRC would manage the parawing technology program with support from MSC. The sailwing technology effort would be managed by MSC with LaRC providing wind tunnel support.
1967 August - -
First flight of Soyuz VI planned for 1968 Nation: USSR. Spacecraft: Soyuz VI. Kozlov was predicting first flight of the VI in 1968, with the first all-up operational flight in 1970.
1967 August 1 - 22:33 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3 Agena D. LV Configuration: SLV-3 Agena D 5805 (AA24) / Agena D 6634. -
Lunar Orbiter 5 Nation: USA. Payload: Lunar Orbiter E. Mass: 389 kg (857 lb). Class: Planetary. Type: Lunar. Spacecraft: Lunar Orbiter. Agency: NASA LaR. COSPAR: 1967-075A. USAF Sat Cat: 2907. Decay Date: 1968-01-31. Lunar Orbiter V was launched from the Eastern Test Range at 6:33 p.m. EDT August 1. The Deep Space Net Tracking Station at Woomera, Australia, acquired the spacecraft about 50 minutes after liftoff. Signals indicated that all systems were performing normally and that temperatures were within acceptable limits. At 12:48 p.m. EDT August 5, Lunar Orbiter V executed a deboost maneuver that placed it in orbit around the moon. The spacecraft took its first photograph of the moon at 7:22 a.m. EDT August 6. Before it landed on the lunar surface on January 31, 1968, Lunar Orbiter V had photographed 23 previously unphotographed areas of the moon's far side, the first photo of the full earth, 36 sites of scientific interest, and 5 Apollo sites for a total of 425 photos.
References: 2, 6, 16, 278.
1967 August 2 - -
Manned spacecraft trainer status Nation: USSR. Program: Lunar L3, Lunar L1, Soyuz. Spacecraft: Soyuz 7K-OK, Soyuz 7K-L1, Soyuz 7K-LOK. The Volga and Soyuz trainers are to be finally operational on 10 and 20 August respectively. The L1 trainer is not progressing and the L3 trainer exists only on paper. The lead cosmonauts have decided to boycott Feoktistov. Nikolayev and Bykovskiy simply refuse to fly with him. They feel Feoktistov's poor vision could result in a catastrophe in a docking attempt, resulting in the death of the crews of both spacecraft involved. The IMBP agrees - 'we can't put an invalid into space'....
References: 376.
1967 August 3 - 07:36 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB ALF-VB-12. -
MPE Barium release Magnetosphere mission Nation: Germany. Agency: NRCC. Apogee: 448 km (278 mi). References: 2.
1967 August 3 - 11:10 GMT - Launch Site: Point Barrow. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.97UM. -
UM Pitot 31 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 155 km (96 mi). References: 2.
1967 August 4 - -
NASA Astronaut Training Group 6 selected. Nation: USA. The group was selected to provide additional scientist-astronauts for Apollo lunar landing and earth-orbit space station missions.. Qualifications: Doctorate in natural sciences, medicine, or engineering. Under 35 years old, under 183 cm height, excellent health. US citizen or willing to become a naturalized citizen.. In response to the poor result of the first scientist-astronaut selection, NASA went ahead with a second round of selections. 923 people applied, of which 69 selected by the National Academy of Sciences for NASA physical and mental evaluation. By the time the new astronauts reported, ambitious Apollo Applications plans had been scrapped, leading to their nickname 'The Excess Eleven'. Seven stayed on through the 1970's and finally got to fly aboard the space shuttle.
1967 August 4 - 03:53 GMT - Launch Site: Woomera. Launch Complex: LA6A. Launch Pad: -. Launch Vehicle: Europa. LV Configuration: Europa I F-6/1. FAILURE: Failure. -
Active first and second stages with dummy third stage and satellite. Nation: Europe. Agency: ELDO. Apogee: 180 km (110 mi). References: 2.
1967 August 4 - 04:53 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.172UG. -
Stellar ultraviolet Ultraviolet / x-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 130 km (80 mi). References: 2.
1967 August 5 - 01:59 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.343GT-UA. -
Recovery test Nation: USA. Agency: NASA. Apogee: 150 km (90 mi). References: 2.
1967 August 5 - 09:56 GMT - Launch Site: Point Barrow. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.290UM. -
UM Pitot 32 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 150 km (90 mi). References: 2.
1967 August 5 - 21:04 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. -
MPE Barium release EXP-32 Aeronomy mission Nation: Germany. Agency: FRG. Apogee: 258 km (160 mi). References: 2.
1967 August 6 - 04:04 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB ALF-VB-13. -
MPE Barium release Magnetosphere mission Nation: Germany. Agency: NRCC. Apogee: 287 km (178 mi). References: 2.
1967 August 7 - 21:44 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thorad SLV-2G Agena D. LV Configuration: Thorad SLV-2G Agena D 510 / Agena D 1637. -
KH-4A 1043 Nation: USA. Payload: KH-4A s/n 1043 / Agena D 1637. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 174 km (108 mi). Apogee: 346 km (214 mi). Inclination: 79.90 deg. Period: 89.70 min. COSPAR: 1967-076A. USAF Sat Cat: 2910. Decay Date: 1967-09-01. KH-4A. Forward camera film came out of the rails on pass 230D. Film degraded past this point. References: 2, 6.
1967 August 8 - -
Gagarin grounded. Nation: USSR. Program: Lunar L1, Soyuz. Spacecraft: Soyuz 7K-L1. The Soviet leadership has decided Gagarin is too important a propaganda asset to take any risks with his life. He is removed from the list of cosmonauts to be selected for space flights, and will be allowed to fly aircraft only with an instructor aboard. This ruling overrules a promise made by Kamanin to Gagarin that he would be put back on the flight rosterthat after he obtained his engineering diploma from the Zhukovskiy Academy on 1 May 1968. A vote is taken of the cosmonaut selection commission on Feoktistov's fitness for duty. The vote is 4:4, but then a quorum of at least 12 commission members is demanded. Feoktistov passes 9:8 in the final vote.
References: 376.
1967 August 8 - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1212. -
FOT GB45 Follow-on Test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1967 August 8 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Combat training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1967 August 8 - 03:28 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL305. -
Solar spectra Solar x-ray and ultraviolet mission Nation: Australia. Agency: WRE/RAE. Apogee: 182 km (113 mi). References: 2.
1967 August 8 - 12:57 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.207UA. -
POGO detector test Ionosphere mission Nation: USA. Agency: NASA. Apogee: 289 km (179 mi). References: 2.
1967 August 8 - 16:05 GMT - Launch Site: Baikonur. Launch Complex: LC162/36. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36-O. LV Configuration: R-36O 8K69 Ya22500 No. 10L. -
Cosmos 171 Nation: USSR. Mass: 1,700 kg (3,700 lb). Class: Military. Type: FOBS. Spacecraft: OGCh. Agency: RVSN. Perigee: 138 km (85 mi). Apogee: 177 km (109 mi). Inclination: 49.60 deg. Period: 87.60 min. COSPAR: 1967-077A. USAF Sat Cat: 2911. Decay Date: 1967-08-08. Fractional Orbital Bombardment system test. References: 2, 6.
1967 August 8 - 21:45 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 CRL AH3.529. -
Extreme ultraviolet Mon Solar extreme ultraviolet mission Nation: USA. Agency: AFCRL. Apogee: 235 km (146 mi). References: 2.
1967 August 8 - 23:56 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.273UI. -
SpE ionosphere Ionosphere mission Nation: USA. Agency: NASA. Apogee: 141 km (87 mi). References: 2.
1967 August 9 - -
Gorbatko grounded. Nation: USSR. Program: Soyuz. Gorbatko shows heart abnormalities in his EKG during a run on the TBK-60 centrifuge. References: 376.
1967 August 9 - 02:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.338CM. -
Vapor trail Aeronomy mission Nation: USA. Agency: NASA. Apogee: 214 km (132 mi). References: 2.
1967 August 9 - 05:45 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1/LC31?. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 172 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: MOM. Perigee: 206 km (128 mi). Apogee: 277 km (172 mi). Inclination: 51.70 deg. Period: 89.30 min. COSPAR: 1967-078A. USAF Sat Cat: 2914. Duration: 8.00 days. Decay Date: 1967-08-17. High resolution photo reconnaissance satellite; returned film capsule References: 2, 6.
1967 August 9 - 07:58 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.340CM. -
Vapor trail Aeronomy mission Nation: USA. Agency: NASA. Apogee: 211 km (131 mi). References: 2.
1967 August 9 - 08:47 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.339CM. -
Vapor trail Aeronomy mission Nation: USA. Agency: NASA. Apogee: 204 km (126 mi). References: 2.
1967 August 9 - 08:47 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.342GM. -
Vapor trail Aeronomy mission Nation: USA. Agency: NASA. Apogee: 158 km (98 mi). References: 2.
1967 August 9 - 09:28 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.341CM. -
Vapor trail Aeronomy mission Nation: USA. Agency: NASA. Apogee: 199 km (123 mi). References: 2.
1967 August 11 - 09:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.223NA. -
LUSTER II 1967 Meteorites mission Nation: USA. Agency: NASA. Apogee: 141 km (87 mi). References: 2.
1967 August 11 - 20:25 GMT - Launch Site: Indian Ocean. Launch Complex: -. Launch Pad: 20.0 S x 65.0 E. Launch Vehicle: M-100. Model: M-100. -
Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 90 km (55 mi). References: 2.
1967 August 12 - 06:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NRL NC3.187. -
Ion Composition Aeronomy / ionosphere mission Nation: USA. Agency: NRL. Apogee: 222 km (137 mi). References: 2.
1967 August 14 - -
Almaz space station schedule approved. Nation: USSR. Spacecraft: Almaz OPS. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On schedule of work on the Almaz space station' was issued. References: 474.
1967 August 14 - -
Gulyayev grounded; Feoktistov in training. Nation: USSR. Program: Soyuz. Cosmonaut Gulyayev has hit his head on a stone when diving in the Kholodniy River. Feoktistov continues his attempt to complete 30 months of command cosmonaut training in 75 days. The makes ten dockings in the Volga trainer - 8 of the are rated as 'bad'. References: 376.
1967 August 15 - -
L3 quarantine discussed. Nation: USSR. Program: Lunar L3. Spacecraft: Soyuz 7K-LOK, LK. Sterilisation and quarantine of the L3 spacecraft on its return from the moon is discussed. References: 376.
1967 August 15 - 18:45 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 CRL AG3.528. -
Extreme ultraviolet Mon Solar extreme ultraviolet mission Nation: USA. Agency: AFCRL. Apogee: 243 km (150 mi). References: 2.
1967 August 16 - 06:36 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL581B. -
Test mission Nation: Australia. Agency: WRE/RAE. Apogee: 152 km (94 mi). References: 2.
1967 August 16 - 17:02 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3B. LV Configuration: Titan IIIB 3B-9. -
OPS 4886 Nation: USA. Payload: KH-8 no. 07 / Agena D. Mass: 3,000 kg (6,600 lb). Class: Surveillance. Type: Military. Spacecraft: KH-8. Agency: NRO/USAF. Perigee: 123 km (76 mi). Apogee: 445 km (276 mi). Inclination: 111.50 deg. Period: 90.10 min. COSPAR: 1967-079A. USAF Sat Cat: 2919. Decay Date: 1967-08-28. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1967 August 17 - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 466. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1967 August 18 - -
Energia Engineer Cosmonaut Training Group 2 selected. Nation: USSR.
1967 August 18 - Launch Site: Green River. Launch Complex: Pad 2. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena D055. -
USAF D055 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1967 August 18 - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena E003. -
USAF E003 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1967 August 21 - 17:59 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 2-52-96. -
X-15A-2 Ramjet/Hycon/TPS Test/Imaging mission? Nation: USA. Agency: NASA/USAF. Apogee: 27 km (16 mi). First test with full ablative coating, ramjet pod. Maximum Speed - 5419 kph. Maximum Altitude - 27740 m. References: 2.
1967 August 23 - 04:41 GMT - Launch Site: Vandenberg. Launch Complex: SLC10W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Burner 2. LV Configuration: Thor Burner 2 266. -
DMSP-Block-4A F9 Nation: USA. Program: DMSP. Payload: DAPP 3419 (FTV-4). Mass: 130 kg (280 lb). Class: Earth. Type: Weather. Spacecraft: DMSP Block 4A. Agency: USAF. Perigee: 818 km (508 mi). Apogee: 873 km (542 mi). Inclination: 98.90 deg. Period: 101.90 min. COSPAR: 1967-080A. USAF Sat Cat: 2920. Defense Meteorological Satellite Program. References: 2, 6.
1967 August 24 - -
Agreement on protecting the earth from contamination by Apollo samples Nation: USA. Program: Apollo. An interagency agreement on protecting the earth's biosphere from lunar sources of contamination was signed by James E. Webb, NASA; John W. Gardiner, HEW; Orville L. Freeman, Department of Agriculture; Stewart L. Udall, Department of Interior; and Frederick Seitz, National Academy of Sciences. The agreement established a committee to advise the NASA Administrator on back contamination and the protection of the biological and chemical integrity of lunar samples, on when and how astronauts and lunar samples might be released from quarantine, and on policy matters.
References: 16.
1967 August 24 - -
Soyuz launch commission. Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Over 200 recommendations were made for revision of the parachute system, and all of these had to be made over the last two to three months. There have been 30 drops of the FAB-3000 Soyuz capsule mass simulator and two drops of capsule mock-ups. The entire series of tests is due to be completed by 20 September. This will allow flight of the first two manned spacecraft on 15 to 20 October. The commission is split over the selection of Feoktistov for the flight. It has to be referred to Smirnov and Ustinov for a final decision.
References: 376.
1967 August 24 - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena D059. FAILURE: Failure. -
USN D059 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 0 km ( mi). References: 2.
1967 August 24 - 04:59 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 173 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 8. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 269 km (167 mi). Apogee: 499 km (310 mi). Inclination: 71.00 deg. Period: 92.20 min. COSPAR: 1967-081A. USAF Sat Cat: 2921. Completed Operations Date: 1967-12-03. Decay Date: 1967-12-17. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1967 August 24 - 10:05 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL521. -
Geocorona? Ultraviolet astronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 178 km (110 mi). References: 2.
1967 August 25 - Launch Site: Green River. Launch Complex: Pad 1. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena D048. -
USAF D048 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1967 August 25 - 20:27 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 3-62-92. -
X-15A Guid/HT/BLN test Nation: USA. Agency: NASA/USAF. Apogee: 25 km (15 mi). Maximum Speed - 5012 kph. Maximum Altitude - 25720 m. References: 2.
1967 August 26 - 04:36 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.187CG. -
LMSC X-ray X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 125 km (77 mi). References: 2.
1967 August 26 - 06:35 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AF07.328. -
Density Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 177 km (109 mi). References: 2.
1967 August 27 - -
Tass announces water landing exercises Nation: USSR. Program: Lunar L1. Class: Manned. Tass announces water landing exercises; Leonov involved. References: 72.
1967 August 29 - 10:01 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL522. -
Geocorona? Ultraviolet astronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 124 km (77 mi). References: 2.
1967 August 30 - Launch Site: Wallops Island. Launch Complex: LA2. Launch Pad: LA2A?. Launch Vehicle: Astrobee. Model: Astrobee 1500. LV Configuration: Astrobee 1500 NASA 16.03GR. -
Radio astronomy mission Nation: USA. Agency: NASA. Apogee: 1,500 km (900 mi). References: 2.
1967 August 30 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. FAILURE: Failure. -
Combat training launch Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1967 August 30 - 17:32 GMT - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. -
ION 1 / 67 Ionosphere mission Nation: Argentina. Agency: CONAE. Apogee: 225 km (139 mi). References: 2.
1967 August 31 - Launch Site: Baikonur. Launch Complex: LC110R. Launch Pad: -. Launch Vehicle: N1. -
N1 launch pad 110 east completed Nation: USSR. Program: Lunar L3. References: 96.
1967 August 31 - -
7K-VI Zvezda program review. Nation: USSR. Spacecraft: Soyuz VI. The 7K-VI military Soyuz was supposed to have been built on the basis of the 7K-OK model, with a first flight in December 1967. After all the problems with the 7K-OK, Kozlov replaced most subsystems and ended up with a basically new spacecraft, the Zvezda, which will have a mass of 6.3 to 6.6 tonnes. Officially first flight was set for the second half of 1968, but Kozlov says that even a flight in 1969 may not be possible. They simply can't meet the 21 July 1967 decree to have the spacecraft in service in 1968 - they need a further 18 to 24 months of development time. In Kamanin's opinion, this whole approach has been mismanaged. Urgent military experiments could have been flying long ago on a series of Voskhod flights. Furthermore there is no trainer yet for the 7K-VI. Kozlov says simply that he is not responsible for providing a trainer. Resort has to be made to a new design bureau set up specifically to produce simulators, headed by Darevskiy.
References: 376.
1967 August 31 - 08:00 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1/LC31?. Launch Vehicle: Soyuz. Model: Molniya 8K78M. -
Cosmos 174 Nation: USSR. Program: Molniya. Payload: Molniya-1. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-1. Agency: MOM. Perigee: 430 km (260 mi). Apogee: 39,796 km (24,728 mi). Inclination: 64.90 deg. Period: 715.00 min. COSPAR: 1967-082A. USAF Sat Cat: 2925. Decay Date: 1968-12-30. Probable commsat failure. Investigation of the upper atmosphere and outer space. References: 2, 6, 64.
1967 August 31 - 22:06 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.43GE. -
Ba clouds Plasma mission Nation: USA. Agency: NASA. Apogee: 321 km (199 mi). References: 2.
1967 August 31 - 22:47 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.46GE. -
Double probe Plasma mission Nation: USA. Agency: NASA. Apogee: 228 km (141 mi). References: 2.
1967 September 1 - -
S-IVB Orbital Workshop mockup returned for a number of design changes. Nation: USA. Spacecraft: Orbital Workshop. MSFC returned a McDonnell Douglas-built S-IVB Orbital Workshop mockup to the contractor's Space Systems Center in Huntington Beach, California, for incorporation of a number of design changes. Following modification, the mockup would represent the S IVB stage as a manned space laboratory designed for use in the AAP. The design changes included relocation of a floor separating two sections of the stage's liquid hydrogen tank, addition of a ceiling and other fixtures, and relocation of some of the experiment stations.
1967 September 1 - Launch Site: Sary Shagan. Launch Complex: LC6. Launch Pad: -. Launch Vehicle: A-35. Model: A-350Zh. -
Phase 1 state trials flight Nation: USSR. Agency: PRO. Apogee: 300 km (180 mi). References: 2.
1967 September 1 - 10:30 GMT - Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. FAILURE: Failure of Block I stage at 296 seconds. Remnants of spacecraft and stage fell near Novaya Zemlya. -
Zenit-2 11F61 s/n 51 Nation: USSR. Payload: Zenit-2 11F61 s/n 51. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: RVSN. COSPAR: F670901A. Decay Date: 1967-09-01. Area survey photo reconnaissance satellite. References: 42,93.
1967 September 2 - 17:37 GMT - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. -
ION 2 / 67 Ionosphere mission Nation: Argentina. Agency: CONAE. Apogee: 232 km (144 mi). References: 2.
1967 September 2 - 20:31 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.44GE. -
4 Barium clouds Plasma mission Nation: USA. Agency: NASA. Apogee: 321 km (199 mi). References: 2.
1967 September 2 - 20:42 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.47GE. -
E fields Plasma mission Nation: USA. Agency: NASA. Apogee: 233 km (144 mi). References: 2.
1967 September 4 - Launch Site: Baikonur. Launch Complex: PU31. Launch Pad: PU31?. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1967 September 6 - -
Apollo spacecraft weight situation serious Nation: USA. Program: Apollo. Spacecraft: Apollo LM. ASPO Manager George Low in a letter to Dale Myers of North American Aviation, emphasized that the spacecraft weight situation was the single most serious problem in the entire Apollo program. Additional Details: Apollo spacecraft weight situation serious. References: 16.
1967 September 6 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1222. -
FOT GB46 Follow-on Test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1967 September 7 - -
LM-1 (Apollo 5) continued to have serious schedule difficulties Nation: USA. Program: Apollo. Spacecraft: Apollo LM. LM-1 (Apollo 5) continued to have serious schedule difficulties. However, all known problems were resolved with the exception of the propulsion system leaks. Leak checks of the ascent stage indicated excessive leaking in the incline oxidizer orifice flange. The spacecraft was approximately 39 days behind the July 18, LM-1 KSC Operations Flow Plan.
References: 16.
1967 September 7 - 05:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AG07.176. -
Density Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 101 km (62 mi). References: 2.
1967 September 7 - 20:34 GMT - Launch Site: Arecibo. Launch Complex: VB. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.308UI. -
Lower ionosphere Ionosphere mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1967 September 7 - 20:34 GMT - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-12 Sandia 152-88. -
LRL BOX-8a X-ray astronomy mission Nation: USA. Agency: Sandia. Apogee: 187 km (116 mi). References: 2.
1967 September 7 - 22:04 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta G. LV Configuration: Thor Delta G 475/D51. -
Biosatellite 2 Nation: USA. Payload: Biosat 2. Mass: 507 kg (1,117 lb). Class: Biology. Spacecraft: Biosatellite. Agency: NASA ARC. Perigee: 297 km (184 mi). Apogee: 318 km (197 mi). Inclination: 33.50 deg. Period: 90.70 min. COSPAR: 1967-083A. USAF Sat Cat: 2935. Decay Date: 1967-09-15. Biological capsule recovered. The scientific payload, consisting of 13 select biology and radiation experiments, was exposed to microgravity during 45 hours of Earth-orbital flight. Experimental biology packages on the spacecraft contained a variety of specimens, including insects, frog eggs, microorganisms and plants. The planned three-day mission was recalled early because of the threat of a tropical storm in the recovery area, and because of a communication problem between the spacecraft and the tracking systems. The primary objective of the Biosatellite II mission was to determine if organisms were more, or less, sensitive to ionizing radiation in microgravity than on Earth. To study this question, an artificial source of radiation was supplied to a group of experiments mounted in the forward part of the spacecraft.
References: 2, 6, 297.
1967 September 8 - -
Reduced Apollo spacecraft delivery schedule approved by NASA HQ Nation: USA. Program: Apollo. A revised spacecraft delivery schedule with a maximum delivery rate of six spacecraft per year as opposed to a delivery rate of one spacecraft every six weeks for the Apollo program was proposed by MSC and approved by NASA Hq. References: 16.
1967 September 8 - -
L1 Expert Commission. Nation: USSR. Program: Lunar L1. Mishin certifies that the spacecraft will be delivered on 13-14 September, so launch is set for the window of 25-27 September. There are two recovery zones: Baikonur is the prime, with the Indian Ocean as secondary in case of a ballistic re-entry. References: 376.
1967 September 8 - Launch Site: Baikonur. Launch Complex: PU32. Launch Pad: PU32?. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1967 September 8 - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena D057. -
USAF D057 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1967 September 8 - 00:07 GMT - Launch Site: Arecibo. Launch Complex: VB. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.305UI. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1967 September 8 - 03:21 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NRL NB3.196. -
Stellar X-ray X-ray astronomy mission Nation: USA. Agency: NRL. Apogee: 200 km (120 mi). References: 2.
1967 September 8 - 07:57 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36B. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3C Centaur. LV Configuration: SLV-3C Centaur AC-13 / Centaur D-1A 5901C. -
Surveyor 5 Nation: USA. Payload: Surveyor SC-5. Mass: 279 kg (615 lb). Class: Planetary. Type: Lunar. Spacecraft: Surveyor. Agency: NASA/JPL. COSPAR: 1967-084A. USAF Sat Cat: 2937. Decay Date: 1967-09-11. Soft lunar landing; returned 19,000 photos, soil data. References: 2, 6, 278.
1967 September 8 - 16:00 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-377. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1967 September 11 - -
Kamanin reviews military space plans for the period 1968-1975. Nation: USSR. Program: Almaz. Spacecraft: Almaz OPS, Soyuz VI, Soyuz 7KT-OK, Spiral OS. The first military combat space units are to be formed - for operations with the 7K-VI and Almaz spacecraft, together with subsidiary Soyuz transport and training flights. References: 376.
1967 September 11 - Launch Site: Vandenberg. Launch Complex: 395-B. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-21. -
Glowing Bright Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). FOT GB44 Follow-on Test launch References: 2.
1967 September 11 - 10:30 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 175 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: MOM. Perigee: 181 km (112 mi). Apogee: 356 km (221 mi). Inclination: 72.80 deg. Period: 89.80 min. COSPAR: 1967-085A. USAF Sat Cat: 2939. Duration: 8.00 days. Decay Date: 1967-09-19. High resolution photo reconnaissance satellite; returned film capsule References: 2, 6.
1967 September 12 - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3TY-1. FAILURE: Failure. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1967 September 12 - 17:00 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 176 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 10. Mass: 250 kg (550 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 196 km (121 mi). Apogee: 1,525 km (947 mi). Inclination: 81.90 deg. Period: 102.20 min. COSPAR: 1967-086A. USAF Sat Cat: 2942. Completed Operations Date: 1967-11-11. Decay Date: 1968-03-03. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1967 September 12 - 20:57 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.45GE. -
Ba clouds, E field Plasma mission Nation: USA. Agency: NASA. Apogee: 321 km (199 mi). References: 2.
1967 September 12 - 20:59 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.48GE. FAILURE: Failure. -
E fields Plasma mission Nation: USA. Agency: NASA. Apogee: 227 km (141 mi). References: 2.
1967 September 13 -
1967 September 13 - -
Kamanin continues work on the 8-year plan for military space. Nation: USSR. Program: Almaz. Spacecraft: Almaz OPS, Soyuz VI, Soyuz 7KT-OK, Spiral OS. The general staff's space plans are impressive - in 1968-1975 they foresee no less than 20 Almaz space stations, 50 military 7K-VI missions, 200 Soyuz training spacecraft flights and 400 Soyuz space transport flights. This is based on the assumption that the crew of the military space stations will have to be rotated every 15 days. That will require 48 transport spacecraft per year, implying not less than 30 ready crews with 3 cosmonauts in each crew (this in turn implies each each cosmonaut will fly a space mission 1.5 times per year). Since supplies will have to be delivered to the stations, that will require another 200 additional transport spacecraft launches. And all of this is aside from civilian Soyuz flights, L1, L3, and various other civilian spacecraft - implying a total of 1000 launches in the period. This will require 800 Soyuz-class launch vehicles, 100 Protons, and 10 to 12 N1 boosters. The inevitable conclusion for Kamanin is that most of the transport launches should be made by a reusable winged spacecraft, air-launched from an An-22 heavy transport. This is the goal of the Spiral project. By 1975 Kamanin sees a requirement for 400 active cosmonauts, organised in two to three aerospace brigades, supported by10 aviation regiments, and including the TsPK training centre -- altogether 20,000 to 25,000 men. 250 million roubles will be needed to build new aerodromes and facilities alone, all chargeable to the VVS. Total cost will run into tens of billions of roubles per year.
References: 376.
1967 September 13 - -
Smirnov told Feoktistov unready for command. Nation: USSR. Program: Soyuz. Vershinin writes a letter to Smirnov on the subject of Feoktistov. He tells Smirnov he is not ready to be a spacecraft commander. References: 376.
1967 September 14 - Launch Site: Green River. Launch Complex: Pad 1. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena D056. -
USAF D056 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1967 September 15 - 19:41 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thorad SLV-2G Agena D. LV Configuration: Thorad SLV-2G Agena D 512 / Agena D 1641. -
KH-4B 1101 Nation: USA. Payload: KH-4B s/n 1101 / Agena D 1641. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4B. Agency: NRO/CIA. Perigee: 156 km (96 mi). Apogee: 372 km (231 mi). Inclination: 80.00 deg. Period: 89.70 min. COSPAR: 1967-087A. USAF Sat Cat: 2946. Decay Date: 1967-10-04. KH-4B. First mission of the KH-4B series. Best film to date. References: 2, 6.
1967 September 16 - -
Apollo CSM 017 guidance and navigation computer locked up Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. During operational checkout procedures on CSM 017, which included running the erasable memory program before running the low-altitude aborts, the guidance and navigation computer accidentally received a liftoff signal and locked up. Investigation was initiated to determine the reason for the liftoff signal and the computer lockup (switch to internal control). No damage was suspected.
References: 16.
1967 September 16 - 06:06 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 177 Nation: USSR. Payload: Zenit-2 11F61 s/n 53. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: MOM. Perigee: 201 km (124 mi). Apogee: 267 km (165 mi). Inclination: 51.70 deg. Period: 89.10 min. COSPAR: 1967-088A. USAF Sat Cat: 2947. Duration: 8.00 days. Decay Date: 1967-09-24. Area survey photo reconnaissance satellite. References: 2, 6,93.
1967 September 17 - Launch Vehicle: UR-700. -
LK-700 manned lunar landing spacecraft authorised Nation: USSR. Spacecraft: LK-700. Development of the LK-700 manned lunar landing spacecraft was undertaken in accordance with decree 1070-363 of the Soviet Ministers and Central Committee of the Communist Party on 17 September 1967 and MOM decree 472 of 28 September 1967. Study index number 4855CC by TsNIIMASH in 1966 showed that any development of improved versions of the N1 would be practically equivalent to design and qualification of a new rocket, while the UR-700 modular approach allowed a range of payloads without requalification. The UR-700/LK-700 combination could support the DLB lunar base better, as well as Venus/Mars manned flybys and Mars landing expeditions. Work would continue through the mock-up stage until 1974.
1967 September 18 - 19:10 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.50GA. -
Thermosphere Aeronomy mission Nation: USA. Agency: NASA. Apogee: 286 km (177 mi). References: 2.
1967 September 19 - -
L1 Launch Commission. Nation: USSR. Program: Lunar L1, Soyuz. Spacecraft: Soyuz 7K-L1. The cosmonauts are training at Area 113, and the launch will be from Area 81. The State Commission meets from 15:00 to 18:30. So far there have been six successful Proton flights and only one failure. The Proton assembly was completed in 71 working days. UR-500 s/n 7 for this launch had 138 systems requiring rework at the launch site and 120 discrepancies (an increase: Proton number 5 for the first L1 launch had 208 reworks/223 discrepancies, while Proton number 6 for the first L1 launch was down to 70 reworks/194 defects). The L1 spacecraft had 15 notable defects on delivery, but this had increased to 100 by the time of the commission. Therefore Mishin should not be certifying readiness for launch. Manned flight to the moon requires a total mission probability of 0.99 to 0.9999, and Mishin puts the current Proton/L1 system reliability at only 0.6. It certainly has to be better- this is an 'all-up mission'. It will be the world's first re-entry at parabolic velocity. On return from the moon the spacecraft has to hit a re-entry corridor only 30 km across. The range of possible touchdown points extends along a 400 km wide corridor stretching from the equator to the North Pole, and extending over the Indian Ocean, India, Central Asia, and Siberia.
References: 376.
1967 September 19 - 14:45 GMT - Launch Site: Baikonur. Launch Complex: LC161/35. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36-O. LV Configuration: R-36O 8K69 Ya22500 No. 14L. -
Cosmos 178 Nation: USSR. Mass: 1,700 kg (3,700 lb). Class: Military. Type: FOBS. Spacecraft: OGCh. Agency: RVSN. Perigee: 138 km (85 mi). Apogee: 258 km (160 mi). Inclination: 49.70 deg. Period: 88.40 min. COSPAR: 1967-089A. USAF Sat Cat: 2951. Decay Date: 1967-09-19. Fractional Orbital Bombardment system test. References: 2, 6.
1967 September 19 - 18:28 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3B. LV Configuration: Titan IIIB 3B-10. -
OPS 4941 Nation: USA. Payload: KH-8 no. 08 / Agena D. Mass: 3,000 kg (6,600 lb). Class: Surveillance. Type: Military. Spacecraft: KH-8. Agency: NRO/USAF. Perigee: 122 km (75 mi). Apogee: 401 km (249 mi). Inclination: 106.00 deg. Period: 89.70 min. COSPAR: 1967-090A. USAF Sat Cat: 2952. Decay Date: 1967-09-30. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1967 September 20 - Launch Vehicle: Saturn I, Saturn V. -
Proposed sequence of Apollo missions leading to a lunar landing mission Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Flight: Apollo 204, Apollo 11, Apollo 12, Apollo 15. MSC proposed to the NASA Office of Manned Space Flight a sequence of missions leading to a lunar landing mission. The sequence included the following basic missions: - A - Saturn V/unmanned CSM development
- B - Saturn IB/unmanned LM development
- C - Saturn IB/manned CSM evaluation
- D - Saturn V/manned CSM and LM development (A dual Saturn IB mission would be an alternative to the Saturn V for mission D)
- E - CSM/LM operations in high earth orbit
- F - Lunar orbit mission
- G - Lunar landing mission (like Apollo 11)
- H - Lunar landing mission (Apollo 12, 13, and 14)
- I - Reserved for lunar survey missions (not used)
- J - Lunar landing missions, upgraded hardware (Apollo 15, 16, and 17)
References: 16.
1967 September 20 - Launch Vehicle: N1, UR-700. -
Review of N1 progress. Nation: USSR. Program: Lunar L3. Spacecraft: Spiral OS, LK-700. The booster was supposed to be launched by 1966, but there is no way it will be finished this year, and it is highly questionable it will even get off the ground in 1968. The N1 tanks are pressurised to 2 atmospheres, and can go up to three atmospheres in an emergency. In the enormous MIK assembly hall are three N1's - one 'iron bird' ground test model and two flight vehicles. The first roll out of the mock-up will take place in 1967, and the first launch attempt is still expected in 1968 (the first launch will not be attempted until the second and third stages complete stand tests. There is no test stand for the first stage, it will be fired for the first time in flight). An explosion would destroy the pad, requiring several years of repairs. There are two pads, but even that would not be a guarantee of the availability of the rocket due to the poor expected initial reliability. The N1 project is costing 10 billion roubles, not including considerable investment required by the military. To Kamanin the whole thing is a boondoggle, showing the necessity for development of lighter air-launched boosters. He believes there are many mistakes in design and construction, but Mishin, Pashkov, Smirnov, and Ustinov support these doubtful projects of Korolev and Mishin, instead of technically sound projects such as Chelomei's UR-700 or MiG's air-launched spacecraft. If Mishin thinks the current Proton/L1 reliability is only 0.6, then that of the completely unproved N1/L3 must be even less...
References: 376.
1967 September 21 - -
L1 launch delayed to November. Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. The L1 in preparation at Area 31 will not be ready for the planned 20 October launch due to delays in qualification of the parachute system at Fedosiya. No launch attempt now expected until November. References: 376.
1967 September 21 - Launch Site: Johnston Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sandhawk. Model: Terrier Sandhawk. LV Configuration: Terrier Sandhawk Sandia 281-7. -
Aeronomy mission Nation: USA. Agency: Sandia. Apogee: 383 km (237 mi). AEC galactic astronomy payload - detected cosmic soft x-rays. References: 2.
1967 September 21 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-101. -
LASL Solar Solar mission Nation: USA. Agency: Sandia. Apogee: 335 km (208 mi). References: 2.
1967 September 21 - Launch Site: Baikonur. Launch Complex: PU33. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1967 September 21 - 07:38 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.45UI. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 768 km (477 mi). References: 2.
1967 September 22 - -
Merger of North American Aviation and Rockwell-Standard Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The merger of North American Aviation, Inc., and Rockwell-Standard Corp. became effective and was announced. The company was organized into two major groups, the Commercial Products Group and the Aerospace and Systems Group. The new company would be known as North American Rockwell and use the acronym NR.
References: 16.
1967 September 22 - 02:28 GMT - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 831. -
FOT GB47 Follow-on Test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1967 September 22 - 14:05 GMT - Launch Site: Baikonur. Launch Complex: LC162/36. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36-O. LV Configuration: R-36O 8K69 Ya22500 No. 15L. -
Cosmos 179 Nation: USSR. Mass: 1,700 kg (3,700 lb). Class: Military. Type: FOBS. Spacecraft: OGCh. Agency: RVSN. Perigee: 139 km (86 mi). Apogee: 207 km (128 mi). Inclination: 49.60 deg. Period: 87.90 min. COSPAR: 1967-091A. USAF Sat Cat: 2962. Decay Date: 1967-09-22. Fractional Orbital Bombardment system test. References: 2, 6.
1967 September 25 - 08:25 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout A. LV Configuration: Scout A S157C. -
Transit O-14 Nation: USA. Program:
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