Chronology - Quarter 3 1975 home
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1975 July 1 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: Pioner.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi). References: 2.
1975 July 1 - Launch Site: Vandenberg. Launch Complex: LF26. Launch Pad: LF26?. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-11.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1975 July 1 - Launch Site: Baikonur. Launch Complex: LC177. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1975 July 3 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 6 AC. LV Configuration: Skylark 6 AC SL1295.
  • Ionosphere mission? Nation: UK. Agency: BAC. Apogee: 270 km (160 mi). References: 2.
1975 July 3 - 13:40 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 748 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 190 km (110 mi). Apogee: 303 km (188 mi). Inclination: 62.80 deg. Period: 89.40 min. COSPAR: 1975-061A. USAF Sat Cat: 8006. Duration: 13.00 days. Decay Date: 1975-07-16. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1975 July 4 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100N. Model: UR-100N. FAILURE: Failure.
  • Operational missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1975 July 4 - 00:56 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53721-259.
  • Cosmos 749 Nation: USSR. Program: Tselina. Mass: 900 kg (1,980 lb). Class: Sigint. Spacecraft: Tselina-O. Agency: MO SSSR. Perigee: 509 km (316 mi). Apogee: 550 km (340 mi). Inclination: 74.00 deg. Period: 95.30 min. COSPAR: 1975-062A. USAF Sat Cat: 8009. Decay Date: 1980-09-26. Replaced Cosmos 610. Possible ELINT satellite. References: 2, 6.
1975 July 8 - 05:05 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M.
  • Molniya 2-13 Nation: USSR. Program: Molniya. Payload: Molniya-2. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-2. Agency: MOM. Perigee: 1,887 km (1,172 mi). Apogee: 38,492 km (23,917 mi). Inclination: 63.90 deg. Period: 718.30 min. COSPAR: 1975-063A. USAF Sat Cat: 8015. Operation of the long-range telephone and telegraph radiocommunications system in the USSR; transmission of television programmes to stations in the Orbita network. References: 2, 6.
1975 July 10 - 08:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.73GG.
  • 13-in RC Flight 4 Astronomy mission Nation: USA. Agency: NASA. Apogee: 179 km (111 mi). References: 2.
1975 July 11 - 04:15 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
  • Meteor 2-01 Nation: USSR. Payload: Meteor-2 no. 1. Mass: 2,750 kg (6,060 lb). Class: Earth. Type: Weather. Spacecraft: Meteor-2. Agency: MOM. Perigee: 844 km (524 mi). Apogee: 876 km (544 mi). Inclination: 81.30 deg. Period: 102.20 min. COSPAR: 1975-064A. USAF Sat Cat: 8026. Acquisition of meteorological information needed for use by the weather service. References: 2, 6.
1975 July 15 -
  • X-24 Flight 54 Nation: USA. Payload: X-24B flight 26. Class: Manned. Type: Spaceplane. Spacecraft: X-24B. Crew: Love Michael. Maximum Speed - 1685 kph. Maximum Altitude - 21180 m. Flight Time - 415 sec. References: 49, 97.
1975 July 15 - 03:35 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5V.
  • Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 503 km (312 mi). References: 2.
1975 July 15 - 12:20 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Soyuz 19 (ASTP) Nation: USSR. Program: ASTP. Payload: Soyuz ASTP s/n 75 (EPSA). Mass: 6,790 kg (14,960 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-TM. Agency: MOM. Perigee: 186 km (115 mi). Apogee: 220 km (130 mi). Inclination: 51.80 deg. Period: 88.50 min. COSPAR: 1975-065A. USAF Sat Cat: 8030. Duration: 5.94 days. Decay Date: 1975-07-21. Crew: Kubasov, Leonov. Flight: Soyuz 19 (ASTP), Apollo (ASTP). Soyuz 19 initial orbital parameters were 220.8 by 185.07 kilometres, at the desired inclination of 51.80°, while the period of the first orbit was 88.6 minutes. On 17 July the two spacecraft docked. The crew members rotated between the two spacecraft and conducted various mainly ceremonial activities. Leonov was on the American side for 5 hours, 43 minutes, while Kubasov spent 4:57 in the command and docking modules.

    After being docked for nearly 44 hours, Apollo and Soyuz parted for the first time and were station-keeping at a range of 50 meters. The Apollo crew placed its craft between Soyuz and the sun so that the diameter of the service module formed a disk which blocked out the sun. After this experiment Apollo moved towards Soyuz for the second docking.

    Three hours later Apollo and Soyuz undocked for the second and final time. The spacecraft moved to a 40 m station-keeping distance so that an ultraviolet absorption experiment could be performed. With all the joint flight activities completed, the ships went on their separate ways. References: 2, 6, 32, 33,60, 452.

1975 July 15 - 19:50 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39B. Launch Pad: -. Launch Vehicle: Saturn I. Model: Saturn IB. LV Configuration: Saturn IB SA-210.
  • Apollo (ASTP) Nation: USA. Program: ASTP. Payload: Apollo CSM 111. Mass: 14,768 kg (32,557 lb). Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo CSM. Location of Spacecraft: California Science Center, Los Angeles, CA. Agency: NASA MSC. Perigee: 152 km (94 mi). Apogee: 166 km (103 mi). Inclination: 51.70 deg. Period: 87.60 min. COSPAR: 1975-066A. USAF Sat Cat: 8032. Duration: 9.06 days. Decay Date: 1975-07-24. Crew: Brand, Slayton, Stafford. Flight: Soyuz 19 (ASTP), Apollo (ASTP). This flight marked the culmination of the Apollo-Soyuz Test Project, a post-moon race 'goodwill' flight to test a common docking system for space rescue. 15 July 1975 began with the flawless launch of Soyuz 19. Apollo followed right on schedule. Despite a stowaway - a 'super Florida mosquito' - the crew accomplished a series of rendezvous manoeuvres over the next day resulting in rendezvous with Soyuz 19. At 11:10 on 17 July the two spacecraft docked. The crew members rotated between the two spacecraft and conducted various mainly ceremonial activities. Stafford spent 7 hours, 10 minutes aboard Soyuz, Brand 6:30, and Slayton 1:35. Leonov was on the American side for 5 hours, 43 minutes, while Kubasov spent 4:57 in the command and docking modules.

    After being docked for nearly 44 hours, Apollo and Soyuz parted for the first time and were station-keeping at a range of 50 meters. The Apollo crew placed its craft between Soyuz and the sun so that the diameter of the service module formed a disk which blocked out the sun. This artificial solar eclipse, as viewed from Soyuz, permitted photography of the solar corona. After this experiment Apollo moved towards Soyuz for the second docking.

    Three hours later Apollo and Soyuz undocked for the second and final time. The spacecraft moved to a 40 m station-keeping distance so that the ultraviolet absorption (UVA MA-059) experiment could be performed. This was an effort to more precisely determine the quantities of atomic oxygen and atomic nitrogen existing at such altitudes. Apollo, flying out of plane around Soyuz, projected monochromatic laser-like beams of light to retro-reflectors mounted on Soyuz. On the 150-meter phase of the experiment, light from a Soyuz port led to a misalignment of the spectrometer, but on the 500-meter pass excellent data were received; on the 1,000-meter pass satisfactory results were also obtained.

    With all the joint flight activities completed, the ships went on their separate ways. On 20 July the Apollo crew conducted earth observation, experiments in the multipurpose furnace (MA-010), extreme ultraviolet surveying (MA-083), crystal growth (MA-085), and helium glow (MA-088). On 21 July Soyuz 19 landed safely in Kazakhstan. Apollo continued in orbit on 22-23 July to conduct 23 independent experiments - including a doppler tracking experiment (MA-089) and geodynamics experiment (MA-128) designed to verify which of two techniques would be best suited for studying plate tectonics from earth orbit.

    After donning their space suits, the crew vented the command module tunnel and jettisoned the docking module. The docking module would continue on its way until it re-entered the earth's atmosphere and burned up in August 1975. References: 2, 6, 33,60, 452.

  • Saturn S-IVB-210 Nation: USA. Program: ASTP. Payload: Saturn S-IVB-210. Agency: NASA MSF. Perigee: 152 km (94 mi). Apogee: 166 km (103 mi). Inclination: 51.70 deg. Period: 87.60 min. COSPAR: 1975-066B. USAF Sat Cat: 8033. Decay Date: 1975-07-16. References: 2, 279.
  • Docking Module 2 Nation: USA. Program: ASTP. Payload: Apollo DM-2. Spacecraft: Apollo ASTP Docking Module. Agency: NASA MSC. Perigee: 201 km (124 mi). Apogee: 222 km (137 mi). Inclination: 51.70 deg. Period: 88.73 min. COSPAR: 1975-066C. USAF Sat Cat: 8042. Decay Date: 1975-08-02. References: 2, 279.
1975 July 16 - 1975 July 17 -
  • ASTP - The 'Handshake in Space'. Nation: USA. Program: ASTP. Flight: Soyuz 19 (ASTP), Apollo (ASTP). Apollo and Soyuz successfully dock and members of the American and Russian crews shake hands in space for the first time. With the Soviet-American détente crumbling, it will be the last such docking for 20 years. Additional Details: ASTP - The 'Handshake in Space'..
1975 July 17 - 09:10 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
  • Cosmos 750 Nation: USSR. Program: DS. Payload: DS-P1-I s/n 15. Mass: 400 kg (880 lb). Class: Military. Type: Target. Spacecraft: DS-P1-I. Agency: MO SSSR. Perigee: 272 km (169 mi). Apogee: 803 km (498 mi). Inclination: 71.00 deg. Period: 95.40 min. COSPAR: 1975-067A. USAF Sat Cat: 8036. Completed Operations Date: 1976-01-30. Decay Date: 1977-09-29. Operational radar target for the ABM forces. References: 2, 6, 99.
1975 July 18 -
  • ASTP-Crew transfers between the docked vehicles. Nation: USA. Program: ASTP. Flight: Soyuz 19 (ASTP), Apollo (ASTP). The crew members take turns visiting each other's capsules, a complicated procedure due to the need to keep both spacecraft manned at all times and for the transfer crews to transition in the docking module between the different Soyuz and Apollo cabin atmospheres. Additional Details: ASTP-Crew transfers between the docked vehicles..
1975 July 19 -
  • ASTP - Joint Apollo/Soyuz flight activities Nation: USA. Program: ASTP. Flight: Soyuz 19 (ASTP), Apollo (ASTP). During day five of the flight, the crews concentrated on docking exercises and experiments that involved the two ships in the undocked mode. During the interval between the first undocking and the second docking, the Apollo crew placed its craft between Soyuz and the sun so that the diameter of the service module formed a disk which blocked out the sun. This artificial solar eclipse, as viewed from Soyuz, permitted Leonov and Kubasov to photograph the solar corona. Additional Details: ASTP - Joint Apollo/Soyuz flight activities.
1975 July 20 - 1975 July 21 -
  • ASTP - Soyuz returns to earth, Apollo remains in orbit. Nation: USSR. Program: ASTP. Flight: Soyuz 19 (ASTP), Apollo (ASTP). Following a rest period of nearly 10 hours, the Soyuz crewmen advised the ground that they were awake and that all systems were normal. The deorbit burn came exactly on time (5:09 in Houston), and the Soyuz crew landed safely in Kazakhstan. For the remaining three and a half days, Stafford, Slayton, and Brand would concentrate on their experiments, but in many respects the saga of Apollo and Soyuz had come to an end.
1975 July 21 - 15:31 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5C. LV Configuration: Black Brant VC NASA 21.25DS.
  • HRTS-1 Solar ultraviolet mission Nation: USA. Agency: NASA. Apogee: 220 km (130 mi). References: 2.
1975 July 21 -
  • Landing of Soyuz 19 (ASTP) Nation: USSR. Program: ASTP. Flight: Soyuz 19 (ASTP), Apollo (ASTP). Soyuz 19 landed safely at 10:51 GMT, 87 km north-east of Arkalyk, 9. 6 km from its aim point.
1975 July 23 -
  • Apollo (ASTP) in-flight experiments Nation: USA. Program: ASTP. Flight: Apollo (ASTP). Some minor experiment hardware problems developed during the final days of the mission, but for the most part the crew members worked through their flight plan - which included 23 independent experiments - with few difficulties. After a relatively quiet day of work on the 22nd, the major part of the 23rd was devoted to preparing for and conducting the doppler tracking experiment (MA-089). The day was also marked by a press conference from space and jettison of the docking module. Additional Details: Apollo (ASTP) in-flight experiments.
1975 July 23 - Launch Vehicle: Shuttle.
  • Shuttle SSME engine chamber Test Nation: USA. The first full thrust chamber test is completed. References: 44.
1975 July 23 - 13:00 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 751 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 197 km (122 mi). Apogee: 313 km (194 mi). Inclination: 62.80 deg. Period: 89.60 min. COSPAR: 1975-068A. USAF Sat Cat: 8040. Duration: 12.00 days. Decay Date: 1975-08-04. Area survey photo reconnaissance satellite; returned film capsule. References: 2, 6.
1975 July 24 - 05:20 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.413GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 120 km (70 mi). References: 2.
1975 July 24 - 19:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53721-254.
  • Cosmos 752 Nation: USSR. Mass: 900 kg (1,980 lb). Class: Calibration. Spacecraft: Taifun-1. Agency: MO SSSR. Perigee: 481 km (298 mi). Apogee: 514 km (319 mi). Inclination: 65.80 deg. Period: 94.50 min. COSPAR: 1975-069A. USAF Sat Cat: 8043. Decay Date: 1981-02-28. Radar calibration mission. References: 2, 6.
1975 July 24 -
  • Landing of Apollo (ASTP) Nation: USA. Program: ASTP. Flight: Apollo (ASTP). Apollo (ASTP) landed at 21:18 GMT, 7.3 km from the recovery ship New Orleans. It was the last splashdown of an American space capsule. However the flight of the last Apollo spacecraft was marred by the fact that the crew almost perished while the capsule was descending under its parachute.

    A failure in switchology led the automatic landing sequence to be not armed at the same time the reaction control system was still active. When the Apollo hadn't begun the parachute deployment sequence by 7,000 metres altitude, Brand hit the manual switches for the apex cover and the drogues. The manual deployment of the drogue chutes caused the CM to sway, and the reaction control system thrusters worked vigorously to counteract that motion. When the crew finally armed the automatic ELS 30 seconds later, the thruster action terminated.

    During that 30 seconds, the cabin was flooded with a mixture of toxic unignited propellants from the thrusters. Prior to drogue deployment, the cabin pressure relief valve had opened automatically, and in addition to drawing in fresh air it also brought in unwanted gases being expelled from the roll thrusters located about 0.6 meter from the relief valve. Brand manually deployed the main parachutes at about 2,700 meters despite the gas fumes in the cabin.

    By the time of splashdown, the crew was nearly unconscious from the fumes, Stafford managed to get an oxygen mask over Brand's face. He then began to come around. When the command module was upright in the water, Stafford opened the vent valve, and with the in-rush of air the remaining fumes disappeared. The crew ended up with a two-week hospital stay in Honolulu. For Slayton, it also meant the discovery of a small lesion on his left lung and an exploratory operation that indicated it was a non-malignant tumour. Additional Details: Landing of Apollo (ASTP).

1975 July 26 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-10W.
  • PAVE PEPPER test Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1975 July 26 - 13:28 GMT - Launch Site: Jiuquan. Launch Complex: LA2B. Launch Pad: -. Launch Vehicle: CZ. Model: FB-1. LV Configuration: Feng Bao 1 701-05.
  • JSSW 3 Nation: China. Payload: JSSW 3. Mass: 1,107 kg (2,440 lb). Class: Surveillance. Type: Military. Spacecraft: JSSW. Agency: MAI. Perigee: 190 km (110 mi). Apogee: 455 km (282 mi). Inclination: 69.00 deg. Period: 90.90 min. COSPAR: 1975-070A. USAF Sat Cat: 8053. Decay Date: 1975-09-14. Photo surveillance; radio transmission. References: 2, 6.
1975 July 26 -
  • Landing of Soyuz 18 Nation: USSR. Program: Salyut. Flight: Soyuz 18. Soyuz 18 landed at 14:18 GMT, 56 km E of Arkalyk.
1975 July 28 - 17:44 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5C. LV Configuration: Black Brant VC NASA 21.29US.
  • Solar ultraviolet mission Nation: USA. Agency: NASA. Apogee: 278 km (172 mi). References: 2.
1975 July 31 - 13:00 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 753 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 181 km (112 mi). Apogee: 330 km (200 mi). Inclination: 62.80 deg. Period: 89.60 min. COSPAR: 1975-071A. USAF Sat Cat: 8059. Duration: 13.00 days. Decay Date: 1975-08-13. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1975 August 5 -
  • X-24 Flight 55 Nation: USA. Payload: X-24B flight 27. Class: Manned. Type: Spaceplane. Spacecraft: X-24B. Crew: Manke. Maximum Speed - 1381 kph. Maximum Altitude - 18290 m. Flight Time - 420 sec. References: 49, 97.
1975 August 7 - Launch Site: Vandenberg. Launch Complex: 395-C. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-52.
  • DG-2 Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1975 August 7 - Launch Site: Kwajalein. Launch Complex: RN. Launch Pad: -. Launch Vehicle: Sergeant. Model: Castor. LV Configuration: Castor-2R.
  • Technology mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1975 August 7 - 03:30 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 CRL A04.308-1.
  • Density / Bremss Aeronomy mission Nation: USA. Agency: USAF CRL. Apogee: 174 km (108 mi). References: 2.
1975 August 7 - 16:10 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.407GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 119 km (73 mi). References: 2.
1975 August 9 - 01:48 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 2913. LV Configuration: Delta 2913 602/D113.
  • COS-B; COS B Nation: Europe. Payload: COS B. Mass: 280 kg (610 lb). Class: Technology. Spacecraft: COS. Agency: ESA. Perigee: 442 km (274 mi). Apogee: 99,002 km (61,516 mi). Inclination: 90.30 deg. Period: 2,203.90 min. COSPAR: 1975-072A. USAF Sat Cat: 8062. Decay Date: 1986-01-18. Eighth CERS/ESRO satellite, first European Space Agency satellite. Launch time 0147:59 GMT. Argument of perigee 344.7 deg. Also registered by the United States in A/AC.105/INF.331 as 1975-72A, category B satellite with orbit 2203.9 min, 442 x 99002 km x 9 0.3 deg. References: 2, 6.
1975 August 12 - Launch Site: Baikonur. Launch Complex: LC173. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1975 August 12 - Launch Site: Baikonur. Launch Complex: LC177. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1975 August 13 - 07:21 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 754 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 326 km (202 mi). Inclination: 71.40 deg. Period: 89.80 min. COSPAR: 1975-073A. USAF Sat Cat: 8069. Duration: 13.00 days. Decay Date: 1975-08-26. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1975 August 14 - 13:29 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53731-288.
  • Cosmos 755 Nation: USSR. Mass: 810 kg (1,780 lb). Class: Navigation. Spacecraft: Parus. Agency: MO SSSR. Perigee: 966 km (600 mi). Apogee: 1,008 km (626 mi). Inclination: 82.90 deg. Period: 104.80 min. COSPAR: 1975-074A. USAF Sat Cat: 8072. Military navigation satellite. References: 2, 6.
1975 August 15 - 04:25 GMT - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • FOT GT122M-1 Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1975 August 15 - 05:21 GMT - Launch Site: Vandenberg. Launch Complex: PLC-C. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.406-2.
  • ESCAPE I (Sphere) Aeronomy mission Nation: USA. Agency: AFSC/CRL. Apogee: 272 km (169 mi). References: 2.
1975 August 16 - Launch Site: Baikonur. Launch Complex: LC106. Launch Pad: -. Launch Vehicle: R-36M.
  • Joint flight trials launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1975 August 16 - 07:40 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.50UH.
  • X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 172 km (106 mi). References: 2.
1975 August 17 - 06:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Pad: -. Launch Vehicle: S. Model: TT-210. LV Configuration: TT-210 TT-210-1F.
  • Test mission Nation: Japan. Agency: NASDA. Apogee: 100 km (60 mi). References: 2.
1975 August 18 - 12:45 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Aries. LV Configuration: Aries NASA 12.26GT-IT.
  • IMS Prototype test Nation: USA. Agency: NASA. Apogee: 417 km (259 mi). References: 2.
1975 August 20 -
  • X-24 Flight 56 Nation: USA. Payload: X-24B flight 28. Class: Manned. Type: Spaceplane. Spacecraft: X-24B. Crew: Love Michael. Maximum Speed - 1625 kph. Maximum Altitude - 21950 m. Flight Time - 420 sec. References: 49, 97.
1975 August 20 - 21:22 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3E. LV Configuration: Titan IIIE 23E-4 / Centaur D-1T E-4.
  • Viking 1 Orbiter Nation: USA. Payload: Viking 1. Mass: 3,399 kg (7,493 lb). Class: Planetary. Type: Mars. Spacecraft: Viking. Agency: NASA JPL. COSPAR: 1975-075A. USAF Sat Cat: 8108. Combined Mars orbiter and lander mission; orbiter inserted in Mars orbit 6/19/76; lander soft landed on Martian surface 7/20/76Mars. Mars Orbit. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
  • Viking 1 Lander Nation: USA. Payload: Viking 1. Class: Planetary. Type: Mars. Spacecraft: Viking. Agency: NASA LaR. COSPAR: 1975-075C. USAF Sat Cat: 9024. Decay Date: 1976-07-20. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1975 August 22 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-13? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1975 August 22 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-13? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1975 August 22 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-13? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1975 August 22 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • SFT-103 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1975 August 22 - 02:11 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
  • Cosmos 756 Nation: USSR. Program: Tselina. Payload: Tselina-D no. 8. Mass: 2,500 kg (5,500 lb). Class: Sigint. Spacecraft: Tselina-D. Agency: MOM. Perigee: 394 km (244 mi). Apogee: 403 km (250 mi). Inclination: 81.20 deg. Period: 92.50 min. COSPAR: 1975-076A. USAF Sat Cat: 8127. Decay Date: 1992-11-05. References: 2, 6.
1975 August 25 -
  • Shuttle Enterprise final assembly. Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise. Start final assembly and closeout system installation, Enterprise (OV-101) References: 15.
1975 August 26 - Launch Site: Baikonur. Launch Complex: LC109. Launch Pad: -. Launch Vehicle: R-36M.
  • Missile accuracy test launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1975 August 26 - 10:40 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-53.
  • Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 351 km (218 mi). References: 2.
1975 August 26 - 18:50 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.74UA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 180 km (110 mi). References: 2.
1975 August 27 - Launch Site: Baikonur. Launch Complex: LC105. Launch Pad: -. Launch Vehicle: R-36M.
  • Joint flight trials launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1975 August 27 - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ.
  • Test mission Nation: USA. Agency: Sandia. Apogee: 10 km (6 mi). References: 2.
1975 August 27 - 01:41 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 2914. LV Configuration: Delta 2914 594/D114.
  • Symphonie 2 Nation: France. Payload: Symphonie MV2. Mass: 398 kg (877 lb). Class: Communications. Spacecraft: Spacebus 100. Agency: CNES/DFV. Perigee: 35,866 km (22,286 mi). Apogee: 35,873 km (22,290 mi). Inclination: 12.70 deg. Period: 1,440.40 min. COSPAR: 1975-077A. USAF Sat Cat: 8132. Completed Operations Date: 1985-01-01. Jointly registered by the Federal Republic of Germany (A/AC.105/INF.329) and France (A/AC.105/INF.330). Symphonie flying model no II. Experimental telecommunications satellite. Orbit: geostationary. Also registered by the United Stat es in A/AC.105/INF.331 as 1975-77A, category C, with orbit 1427.4 min, 35364 x 35870 km x 0.0 deg Positioned in geosynchronous orbit over the Atlantic Ocean at 11 deg W in 1975-1985 As of 1 September 2001 located at 164.06 deg W drifting at 1.071 deg W per day. As of 2007 Mar 8 located at 167.97E drifting at 1.046W degrees per day. References: 2, 6.
1975 August 27 - 14:45 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 757 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 182 km (113 mi). Apogee: 316 km (196 mi). Inclination: 62.80 deg. Period: 89.50 min. COSPAR: 1975-078A. USAF Sat Cat: 8147. Duration: 13.00 days. Decay Date: 1975-09-09. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1975 August 29 - Launch Site: Vandenberg. Launch Complex: LF08. Launch Pad: -. Launch Vehicle: Minuteman 3.
  • FOT GT49GM Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1975 August 29 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-14? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1975 August 29 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-14? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1975 August 30 - 04:10 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-310. LV Configuration: S-310-2.
  • Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 191 km (118 mi). References: 2.
1975 September 2 - 05:40 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5V.
  • Vertikal-3 Solar Ultraviolet/Solar X-ray mission Nation: USSR. Agency: AN SSSR. Apogee: 502 km (311 mi). References: 2.
1975 September 2 - 12:00 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-51.
  • Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 311 km (193 mi). References: 2.
1975 September 2 - 13:09 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M.
  • Molniya 1-31 Nation: USSR. Program: Molniya. Payload: Molniya-1. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-1. Agency: MOM. Perigee: 633 km (393 mi). Apogee: 40,598 km (25,226 mi). Inclination: 62.90 deg. Period: 735.60 min. COSPAR: 1975-079A. USAF Sat Cat: 8187. Decay Date: 1985-11-19. Uncertain if Molniya-1T model was Molniya-1 or Molniya-1T. Operation of the long-range telephone and telegraph radiocommunications system in the USSR; transmission of television programmes to stations in the Orbita network. References: 2, 6.
1975 September 3 - 10:30 GMT - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-12 Sandia 152-?.
  • LRL ACS-1D X-ray astronomy mission Nation: USA. Agency: Sandia. Apogee: 270 km (160 mi). References: 2.
1975 September 4 - 16:35 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Plasma mission Nation: USSR. Apogee: 170 km (100 mi). References: 2.
1975 September 5 -
  • Enterprise aft fuselage complete. Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise. Aft fuselage on dock, Palmdale, Enterprise (OV-101) References: 15.
1975 September 5 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. Model: UR-100K. FAILURE: Failure.
  • Operational missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1975 September 5 - 04:25 GMT - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • ERCS GIANT MOON 7 Communications mission Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1975 September 5 - 14:50 GMT - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 758 Nation: USSR. Payload: Yantar-2K s/n 3. Mass: 6,600 kg (14,500 lb). Class: Surveillance. Type: Military. Spacecraft: Yantar-2K. Agency: MOM. Perigee: 174 km (108 mi). Apogee: 326 km (202 mi). Inclination: 67.10 deg. Period: 89.50 min. COSPAR: 1975-080A. USAF Sat Cat: 8191. Duration: 1.00 days. Decay Date: 1975-09-25. Third Yantar-2K second generation reconnaissance flight, the first with the new Kondor attitude control system. This system experienced problems and failed on the second day of flight. The spacecraft's destruct package was activated by ground command and the spacecraft was destroyed on 6 September 1975 in its second day of flight. References: 2, 6, 69.
1975 September 8 - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P136H.
  • Atomic oxygen Atmospheric mission Nation: UK. Agency: SRC. Apogee: 141 km (87 mi). References: 2.
1975 September 9 -
  • X-24 Flight 57 Nation: USA. Payload: X-24B flight 29. Class: Manned. Type: Spaceplane. Spacecraft: X-24B. Crew: Dana. Maximum Speed - 1593 kph. Maximum Altitude - 21640 m. Flight Time - 435 sec. References: 49, 97.
1975 September 9 - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P168H.
  • Airglow Atmospheric mission Nation: UK. Agency: SRC. Apogee: 130 km (80 mi). References: 2.
1975 September 9 - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P153H.
  • Electron density Ionosphere mission Nation: UK. Agency: SRC. Apogee: 129 km (80 mi). References: 2.
1975 September 9 - 00:19 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M.
  • Molniya 2-14 Nation: USSR. Program: Molniya. Payload: Molniya-2. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-2. Agency: MOM. Perigee: 1,840 km (1,140 mi). Apogee: 38,534 km (23,943 mi). Inclination: 64.00 deg. Period: 718.20 min. COSPAR: 1975-081A. USAF Sat Cat: 8195. Continued operation of the long-range telephone and telegraph radio-communication system within the Soviet Union and transmission of USSR central television programmes to stations in the Orbita and participating international networks (international cooperation scheme). References: 2, 6.
1975 September 9 - 05:30 GMT - Launch Site: Tanegashima. Launch Complex: N. Launch Pad: -. Launch Vehicle: Delta. Model: N-1. LV Configuration: N-1 N-1(F).
  • Kiku 1 Nation: Japan. Payload: ETS 1 (JETS). Mass: 85 kg (187 lb). Class: Technology. Spacecraft: ETS. Agency: NASDA. Perigee: 975 km (605 mi). Apogee: 1,103 km (685 mi). Inclination: 47.00 deg. Period: 106.00 min. COSPAR: 1975-082A. USAF Sat Cat: 8197. JETS-1 (Japanese Engineering Test Satellite -1, national name 'Kiku') is intended for preliminary experiments for confirmation of the launching technologies, acquiring the satellite tracking and control technologies, and for extension tests of the extenda ble antennas, measurement of satellite environment, measurement of satellite attitudes, etc. Launch time 0530 GMT. References: 2, 6.
1975 September 9 - 18:39 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3E. LV Configuration: Titan IIIE 23E-3 / Centaur D-1T E-3.
  • Viking 2 Orbiter Nation: USA. Mass: 3,399 kg (7,493 lb). Class: Planetary. Type: Mars. Spacecraft: Viking. Agency: NASA JPL. COSPAR: 1975-083A. USAF Sat Cat: 8199. Combined Mars orbiter and lander mission; orbiter inserted in Mars orbit 8/7/76; lander soft landed on Martian surface 9/3/76Mars. Mars Orbit. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
  • Viking 2 Lander Nation: USA. Class: Planetary. Type: Mars. Spacecraft: Viking. Agency: NASA LaR. COSPAR: 1975-083C. USAF Sat Cat: 9408. Decay Date: 1976-08-31. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1975 September 9 - 19:32 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Hawk. LV Configuration: Nike Hawk NASA 12.28WT.
  • Test / aeronomy mission Nation: USA. Agency: NASA. Apogee: 162 km (100 mi). References: 2.
1975 September 10 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • SFT-104 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1975 September 11 - 20:40 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Plasma mission Nation: USSR. Apogee: 159 km (98 mi). References: 2.
1975 September 12 - 05:30 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 759 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MT. Agency: MOM. Perigee: 231 km (143 mi). Apogee: 276 km (171 mi). Inclination: 62.80 deg. Period: 89.60 min. COSPAR: 1975-084A. USAF Sat Cat: 8275. Duration: 11.00 days. Decay Date: 1975-09-23. Military topography satellite; returned film capsule; separated science capsule. References: 2, 6.
1975 September 16 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • FOT GT123M-1 Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1975 September 16 - 09:00 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 760 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 174 km (108 mi). Apogee: 335 km (208 mi). Inclination: 65.00 deg. Period: 89.60 min. COSPAR: 1975-085A. USAF Sat Cat: 8281. Duration: 14.00 days. Decay Date: 1975-09-30. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1975 September 17 - 07:10 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53746-311.
  • Cosmos 761 Nation: USSR. Program: Strela. Payload: Strela-1M no. 97. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,400 km (800 mi). Apogee: 1,482 km (920 mi). Inclination: 74.00 deg. Period: 114.70 min. COSPAR: 1975-086A. USAF Sat Cat: 8285. References: 2, 6.
  • Cosmos 762 Nation: USSR. Program: Strela. Payload: Strela-1M no. 98. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,438 km (893 mi). Apogee: 1,485 km (922 mi). Inclination: 74.00 deg. Period: 115.10 min. COSPAR: 1975-086B. USAF Sat Cat: 8286. References: 2, 6.
  • Cosmos 763 Nation: USSR. Program: Strela. Payload: Strela-1M no. 99. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,474 km (915 mi). Apogee: 1,510 km (930 mi). Inclination: 74.00 deg. Period: 115.80 min. COSPAR: 1975-086C. USAF Sat Cat: 8287. References: 2, 6.
  • Cosmos 764 Nation: USSR. Program: Strela. Payload: Strela-1M no. 100. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,479 km (919 mi). Apogee: 1,526 km (948 mi). Inclination: 74.00 deg. Period: 116.00 min. COSPAR: 1975-086D. USAF Sat Cat: 8288. References: 2, 6.
  • Cosmos 765 Nation: USSR. Program: Strela. Payload: Strela-1M no. 101. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,478 km (918 mi). Apogee: 1,550 km (960 mi). Inclination: 74.00 deg. Period: 116.30 min. COSPAR: 1975-086E. USAF Sat Cat: 8289. References: 2, 6.
  • Cosmos 766 Nation: USSR. Program: Strela. Payload: Strela-1M no. 102. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,418 km (881 mi). Apogee: 1,484 km (922 mi). Inclination: 74.00 deg. Period: 114.90 min. COSPAR: 1975-086F. USAF Sat Cat: 8290. References: 2, 6.
  • Cosmos 767 Nation: USSR. Program: Strela. Payload: Strela-1M no. 103. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,455 km (904 mi). Apogee: 1,487 km (923 mi). Inclination: 74.00 deg. Period: 115.40 min. COSPAR: 1975-086G. USAF Sat Cat: 8291. References: 2, 6.
  • Cosmos 768 Nation: USSR. Program: Strela. Payload: Strela-1M no. 104. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,471 km (914 mi). Apogee: 1,491 km (926 mi). Inclination: 74.00 deg. Period: 115.60 min. COSPAR: 1975-086H. USAF Sat Cat: 8292. References: 2, 6.
1975 September 18 - 00:12 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
  • Meteor 1-22 Nation: USSR. Payload: Meteor M no. 22. Mass: 3,800 kg (8,300 lb). Class: Earth. Type: Weather. Spacecraft: Meteor M. Agency: MOM. Perigee: 800 km (490 mi). Apogee: 909 km (564 mi). Inclination: 81.30 deg. Period: 102.00 min. COSPAR: 1975-087A. USAF Sat Cat: 8293. Acquisition of meteorological information needed for use by the weather service. References: 2, 6.
1975 September 18 - 19:47 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.304-1.
  • NMS Aeronomy mission Nation: USA. Agency: USAF CRL. Apogee: 128 km (79 mi). References: 2.
1975 September 19 - Launch Site: Johnston Island. Launch Complex: LE2. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2J. LV Configuration: Thor DSV-2J 201.
  • DG-5 Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). References: 2.
1975 September 19 - 05:15 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.304-2.
  • NMS Aeronomy mission Nation: USA. Agency: USAF CRL. Apogee: 128 km (79 mi). References: 2.
1975 September 21 -
  • Franco-Soviet space cooperation approved. Nation: USSR. Decree 'On USSR-France co-operation In space' was issued. References: 474.
1975 September 23 -
  • X-24 Flight 58 Nation: USA. Payload: X-24B flight 30. Class: Manned. Type: Spaceplane. Spacecraft: X-24B. Crew: Dana. Last rocket-powered flight. Maximum Speed - 1255 kph. Maximum Altitude - 17680 m. Flight Time - 438 sec. References: 49, 97.
1975 September 23 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OSL Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1975 September 23 - 10:00 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 769 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 203 km (126 mi). Apogee: 307 km (190 mi). Inclination: 72.80 deg. Period: 89.60 min. COSPAR: 1975-088A. USAF Sat Cat: 8322. Duration: 12.00 days. Decay Date: 1975-10-05. Area survey photo reconnaissance satellite; returned film capsule. Third successful test of SpK small film return capsule planned for Yantar. SpK capsule FEU-170-13 No. 5L successfully recovered. References: 2, 6, 69.
  • Cosmos 769 Nauka Nation: USSR. Payload: FEU-170-13 s/n 5L. Class: Earth. Type: Magnetosphere. Spacecraft: Nauka. Agency: RVSN. COSPAR: 1975-088xx. References: 2, 279.
1975 September 23 - 10:02 GMT - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-12 Sandia 152-?.
  • LRL ACS-1E X-ray astronomy mission Nation: USA. Agency: Sandia. Apogee: 270 km (160 mi). References: 2.
1975 September 23 - 12:00 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-52.
  • Soft X-ray X-ray astronomy mission Nation: Japan. Agency: ISAS. Apogee: 336 km (208 mi). References: 2.
1975 September 24 - 05:00 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 10. LV Configuration: Kappa 10 K-10-11.
  • X-ray astronomy / solar ultraviolet mission Nation: Japan. Agency: ISAS. Apogee: 196 km (121 mi). References: 2.
1975 September 24 - 12:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53721-260.
  • Cosmos 770 Nation: USSR. Mass: 650 kg (1,430 lb). Spacecraft: Sfera. Agency: MO SSSR. Perigee: 1,165 km (723 mi). Apogee: 1,208 km (750 mi). Inclination: 83.00 deg. Period: 109.10 min. COSPAR: 1975-089A. USAF Sat Cat: 8325. Investigation of the upper atmosphere and outer space. References: 2, 6.
1975 September 24 - 21:27 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.163UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 273 km (169 mi). References: 2.
1975 September 24 - 23:00 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1975 September 25 - 09:50 GMT - Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 771 Nation: USSR. Program: Resurs. Payload: Zenit-4MKT no. 1. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MKT. Agency: MOM. Perigee: 203 km (126 mi). Apogee: 219 km (136 mi). Inclination: 81.30 deg. Period: 88.70 min. COSPAR: 1975-090A. USAF Sat Cat: 8327. Duration: 13.00 days. Decay Date: 1975-10-08. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation. References: 2, 6, 103.
1975 September 26 - 00:17 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36B. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3D Centaur. LV Configuration: SLV-3D Centaur AC-36 / Centaur D-1AR 5016.
  • Intelsat 4A F-1 Nation: International. Program: Intelsat. Mass: 1,500 kg (3,300 lb). Class: Communications. Spacecraft: Intelsat 4A. Agency: Intelsat. Perigee: 35,860 km (22,280 mi). Apogee: 35,910 km (22,310 mi). Inclination: 8.90 deg. Period: 1,441.10 min. COSPAR: 1975-091A. USAF Sat Cat: 8330. Completed Operations Date: 1986-07-24. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit over the Atlantic Ocean at 25 deg W in 1975-1981; over the Atlantic Ocean 18.5 deg W in 1982-1983; over the Atlantic Ocean 30 deg W in 1983-1986 As of 30 August 2001 located at 4.05 deg E drifting at 1.213 deg W per day. As of 2007 Mar 10 located at 28.51E drifting at 1.239W degrees per day. References: 2, 6, 278.
1975 September 27 - 08:37 GMT - Launch Site: Kourou. Launch Complex: Diamant. Launch Pad: -. Launch Vehicle: Diamant. Model: Diamant BP.4. LV Configuration: Diamant BP.4 No. 3.
  • Aura Nation: France. Payload: D-2. Mass: 115 kg (253 lb). Class: Earth. Type: Geodetic. Spacecraft: D. Agency: CNES. Perigee: 476 km (295 mi). Apogee: 697 km (433 mi). Inclination: 37.10 deg. Period: 96.50 min. COSPAR: 1975-092A. USAF Sat Cat: 8332. Decay Date: 1982-09-30. Solar UV radiation experiments. Study of solar and stellar ultraviolet radiation. 1. Spectral analysis of small and large sources located close to the plane of the ecliptic. Responsible organization: Laboratoire d'Astronomie Spatiale, Traverse du Siphon, 13000- Marseille (France). 2. St udy of solar ultraviolet radiation and its absorption by the earth's atmosphere. Responsible organization: Laboratoire de Physique Stellaire et Planetaire, Meudon, France. Weight 106.6 kg. References: 2, 6.
1975 September 29 - Launch Site: Baikonur. Launch Complex: LC103. Launch Pad: -. Launch Vehicle: R-36M.
  • Joint flight trials launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1975 September 29 - 04:15 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 772 Nation: USSR. Program: Salyut 6. Payload: Soyuz 7K-S s/n 2L. Mass: 6,750 kg (14,880 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-S. Agency: MOM. Perigee: 154 km (95 mi). Apogee: 245 km (152 mi). Inclination: 51.80 deg. Period: 88.40 min. COSPAR: 1975-093A. USAF Sat Cat: 8338. Duration: 3.99 days. Decay Date: 1975-10-02. Unmanned military Soyuz 7K-S test flight. Recovered October 3, 1975 4:10 GMT. Unsuccessful mission. Transmitted only on 166 MHz frequency, at none of the other usual Soyuz wavelengths.
    Maneuver Summary:
    193 km X 270 km orbit to 195 km X 300 km orbit. Delta V: 8 m/s
    196 km X 300 km orbit to 196 km X 328 km orbit. Delta V: 8 m/s
    Total Delta V: 16 m/s References: 2, 6, 21, 121.
1975 September 30 -
  • Charles Kowal's Discovery of Jupiter Moon Themisto Nation: USA.
1975 September 30 - Launch Site: Marambio. Launch Complex: -. Launch Pad: -. Launch Vehicle: Canopus. Model: Castor (A).
  • Ionosphere mission Nation: Germany. Agency: MPE. Apogee: 400 km (240 mi). References: 2.
1975 September 30 - 10:02 GMT - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • SFT-05 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1975 September 30 - 18:38 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53721-258.
  • Cosmos 773 Nation: USSR. Program: Strela. Mass: 750 kg (1,650 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-2M. Agency: MO SSSR. Perigee: 772 km (479 mi). Apogee: 790 km (490 mi). Inclination: 74.10 deg. Period: 100.50 min. COSPAR: 1975-094A. USAF Sat Cat: 8343. References: 2, 6.

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