1974 July 1 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100N. Model: UR-100N. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1974 July - -
Soyuz 7K-S cancelled; Soyuz 7K-ST continued Nation: USSR. Spacecraft: Soyuz 7K-S, Soyuz OB-VI, Soyuz T. The 7K-S was cancelled at the same time as the N1 and the reorganisation of the space industry. Experiments planned for the solo flights were transferred to the Salyut program. The first test vehicle was already at Baikonur being prepared for launch. It was decided to launch the first three unmanned as technology tests - Cosmos 670 (7K-S No.1), Cosmos 772 (7K-S No.2), and Cosmos 869 (7K-S No.3). The Soyuz 7K-ST transport project continued, except now being redesigned for a crew of three. The 7K-ST would eventually fly as the Soyuz T and Soyuz TM ferry to the Salyut 7 and Mir space stations.
1974 July - -
FDL-8 lifting body configuration selected for the X-24C. Nation: USA. Spacecraft: X-24C. NASA and the Air Force selected the FDL-8 lifting body configuration for the X-24C. Two versions of the hypersonic aerospacecraft were proposed: one with cheek air intakes and air-breathing engines, and one with the XLR-99 rocket engine of the X-15. Two X-24C were to be built under a $ 200 million budet. They would fly 200 flights over ten years, reaching a maximum speed of Mach 8 and being able to cruise at over Mach 6 for 40 seconds.
1974 July 2 - 12:16 GMT - Launch Site: Sonde Stromfjord. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.156IE-UE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 236 km (146 mi). References: 2.
1974 July 3 - 18:51 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511. -
Soyuz 14 Nation: USSR. Program: Almaz. Payload: Soyuz 7K-T(A9) s/n 62. Mass: 6,800 kg (14,900 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-T/A9. Agency: MOM. Perigee: 195 km (121 mi). Apogee: 217 km (134 mi). Inclination: 51.60 deg. Period: 88.60 min. COSPAR: 1974-051A. USAF Sat Cat: 7361. Duration: 15.73 days. Decay Date: 1974-07-19. Crew: Artyukhin, Popovich. Flight: Soyuz 14. On 4 July Soyuz 14 docked with the Salyut 3 space station after 15 revolutions of the earth. The planned experimental program included manned military reconnaissance of the earth's surface, assessing the fundamental value of such observations, and some supplemental medico-biological research. After the crew's return research continued in the development of the on-board systems and the principles of remote control of such a station.
References: 2, 6, 32, 33, 60, 445.
1974 July 4 - Launch Site: Baikonur. Launch Complex: LC109. Launch Pad: -. Launch Vehicle: R-36M. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1974 July 4 - 00:30 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.433GE. -
Solar cosmic rays Plasma mission Nation: USA. Agency: NASA. Apogee: 140 km (80 mi). References: 2.
1974 July 5 - 15:32 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.488GE. -
Solar cosmic rays Plasma mission Nation: USA. Agency: NASA. Apogee: 141 km (87 mi). References: 2.
1974 July 8 - Launch Site: Sonde Stromfjord. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.157IE-UE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1974 July 9 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2. -
FOT GT120M Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1974 July 9 - 14:40 GMT - Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M. -
Meteor 1-18 Nation: USSR. Payload: Meteor-Priroda no. 1. Mass: 3,800 kg (8,300 lb). Class: Earth. Type: Weather. Spacecraft: Meteor-Priroda. Agency: MOM. Perigee: 883 km (548 mi). Apogee: 909 km (564 mi). Inclination: 81.20 deg. Period: 102.90 min. COSPAR: 1974-052A. USAF Sat Cat: 7363. Conducted experimental work in studying the natural resources of the earth. Also tested plasma engine References: 2, 6.
1974 July 11 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. -
ABRES/SAMAST re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1974 July 11 - 10:59 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. FAILURE: First stage failed 84 seconds after launch. -
DS-P1-Yu s/n 68 Nation: USSR. Program: DS. Payload: DS-P1-Yu. Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: RVSN. COSPAR: F740711A. Development of systems for air defence and the control of outer space. References: 2.
1974 July 12 - 12:50 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 666 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 181 km (112 mi). Apogee: 328 km (203 mi). Inclination: 62.80 deg. Period: 89.60 min. COSPAR: 1974-053A. USAF Sat Cat: 7367. Duration: 13.00 days. Decay Date: 1974-07-25. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1974 July 14 - Launch Site: Jiuquan. Launch Complex: LA2B. Launch Pad: -. Launch Vehicle: CZ. Model: FB-1. LV Configuration: Feng Bao 1 701-04. FAILURE: Vehicle lost attitude stability and destroyed by range safety. -
JSSW 2 Nation: China. Payload: JSSW 2. Spacecraft: JSSW. Agency: PRC. COSPAR: F740714A. References: 279.
1974 July 14 - 05:17 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F/PTS. LV Configuration: Atlas F/PTS 69F. -
NTS 1 Nation: USA. Program: Navstar. Payload: Timation 3. Mass: 293 kg (645 lb). Class: Technology. Type: Navigation. Spacecraft: NTS. Agency: USAF. Perigee: 13,446 km (8,354 mi). Apogee: 13,774 km (8,558 mi). Inclination: 125.20 deg. Period: 468.70 min. COSPAR: 1974-054A. USAF Sat Cat: 7369. Demonstrated navigation technologies leading eventually to Navstar/GPS system. Operated for 5 years. References: 2, 6, 278.
1974 July 16 - 11:51 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout D-1. LV Configuration: Scout D-1-F S186C. -
Aeros 2 Nation: Germany. Payload: Aeros B. Mass: 127 kg (279 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Aeros. Agency: DFVLR. Perigee: 224 km (139 mi). Apogee: 869 km (539 mi). Inclination: 97.50 deg. Period: 95.60 min. COSPAR: 1974-055A. USAF Sat Cat: 7371. Decay Date: 1975-09-25. Upper atmospheric research. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1974 July 16 - 14:59 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3T. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1974 July 17 - -
Shuttle propulsion test article assembly starts. Nation: USA. Program: STS. Start long-lead fabrication (MPTA-098) References: 15.
1974 July 18 - Launch Vehicle: Shuttle. -
Shuttle carrier aircraft purchased Nation: USA. NASA purchases used American Airlines 747 N9668 for use as a carrier to ferry the shuttle orbiter between factory, landing sites, and launch sites. Modification of a 747 to carry the orbiter on its back was chosen over two more costly alternatives that would have suspended it from a wing connecting two fuselages: a new design proposed by NASA LaRC, and a Lockheed proposal for two C-5A transports joined together.
References: 44.
1974 July 18 - Launch Site: Kwajalein. Launch Complex: Meck. Launch Pad: -. Launch Vehicle: Spartan. -
Safeguard TRM-133 Interceptor mission Nation: USA. Agency: USA. Apogee: 100 km (60 mi). References: 2.
1974 July 18 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. -
SSTTP M2-146 Target mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1974 July 19 - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Hydac. -
Low Light TV Technology mission Nation: USA. Agency: SAMSO. Apogee: 150 km (90 mi). References: 2.
1974 July 19 - -
Landing of Soyuz 14 Nation: USSR. Program: Almaz. Flight: Soyuz 14. All objectives were successfully completed and the spacecraft was recovered at 12:21 GMT, landing within 2 km of the aim point 140 km SE of Dzkezkazgan.
1974 July 20 - 06:10 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.84UG. -
Astronomy mission Nation: USA. Agency: NASA. Apogee: 195 km (121 mi). References: 2.
1974 July 22 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL1292. -
Ionosphere mission? Nation: UK. Agency: BAC. Apogee: 210 km (130 mi). References: 2.
1974 July 23 - 01:23 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. -
Molniya 2-10 Nation: USSR. Program: Molniya. Payload: Molniya-2. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-2. Agency: MOM. Perigee: 1,501 km (932 mi). Apogee: 38,868 km (24,151 mi). Inclination: 64.50 deg. Period: 718.10 min. COSPAR: 1974-056A. USAF Sat Cat: 7376. 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.
1974 July 25 - 07:00 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 667 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 176 km (109 mi). Apogee: 320 km (190 mi). Inclination: 65.00 deg. Period: 89.50 min. COSPAR: 1974-057A. USAF Sat Cat: 7383. Duration: 13.00 days. Decay Date: 1974-08-07. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1974 July 25 - 12:00 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 668 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 74. Mass: 400 kg (880 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 270 km (160 mi). Apogee: 494 km (306 mi). Inclination: 71.00 deg. Period: 92.20 min. COSPAR: 1974-058A. USAF Sat Cat: 7385. Completed Operations Date: 1975-02-17. Decay Date: 1975-02-21. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1974 July 26 - Launch Site: Baikonur. Launch Complex: LC140/18. Launch Pad: -. Launch Vehicle: R-36M. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1974 July 26 - 07:00 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 669 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 207 km (128 mi). Apogee: 229 km (142 mi). Inclination: 81.30 deg. Period: 88.80 min. COSPAR: 1974-059A. USAF Sat Cat: 7389. Duration: 13.00 days. Decay Date: 1974-08-08. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule. References: 2, 6.
-
Nauka Cosmos 669 Nation: USSR. Payload: Nauka. Spacecraft: Nauka. Agency: MOM. Perigee: 198 km (123 mi). Apogee: 221 km (137 mi). Inclination: 81.30 deg. Period: 88.69 min. COSPAR: 1974-059G. USAF Sat Cat: 7404. Decay Date: 1974-08-11. References: 2, 279.
1974 July 26 - 15:23 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3T. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1974 July 29 - 12:00 GMT - Launch Site: Baikonur. Launch Complex: LC81/24. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM. LV Configuration: Proton-K/DM 287-01. -
Molniya 1-S Nation: USSR. Program: Molniya. Payload: Molniya 1 s/n 38. Mass: 800 kg (1,760 lb). Class: Communications. Spacecraft: Molniya-1. Agency: MOM. Perigee: 35,738 km (22,206 mi). Apogee: 35,848 km (22,274 mi). Inclination: 14.80 deg. Period: 1,436.40 min. COSPAR: 1974-060A. USAF Sat Cat: 7392. Completed Operations Date: 1974-07-01. Evidently a unique experimental satellite. Arrangements for experimental television broadcasts and establishment of long-range radio-communications. As of 29 August 2001 located at 104.72 deg E drifting at 0.115 deg W per day. As of 2007 Mar 10 located at 41.05E drifting at 0.029W degrees per day.
References: 2, 6, 274.
1974 July 30 - -
Kozlov given own design bureau in Samara. Nation: USSR. Military-Industrial Commission (VPK) Decree 'On separation of TsSKB from NPO Energia and creation of the Volzhkiy Branch' was issued. After the fall of Mishin, Kozlov was offered the Chief Designer job. He rejected it and Glushko was made head of a reorganised NPO Energia. KB Kozlov itself was made a separate entity with the name of Central Specialised Construction Bureau.
References: 474.
1974 August 1 - Launch Vehicle: Energia, RLA. -
New heavy-lift vehicle Nation: USSR. Spacecraft: Buran. Glushko's first action was to implement a decision of the leadership to develop a completely new heavy-lift launch vehicle. This work started in 1974, with a planned first flight in 1984, at a total estimated cost of 5 to 6 billion roubles. One factor in the decision was the fact that Keldysh was greatly disturbed by the manoeuvrability of the space shuttle. He talked the matter up until he managed to get Ustinov and Brezhnev worked as well. He told them a US shuttle could manoeuvre around Soviet PVO and PKO anti-missile and satellite defences and deliver a 25 tonne nuclear bomb of greater than 25 megatons force directly on Moscow. Keldysh was convinced that the US planned to use the shuttle for a pre-emptive nuclear strike on Russia. Therefore the USSR needed an analogous capability to maintain the strategic balance. While this discussion was going on, the energies of TsKBEM were completely absorbed in the Apollo-Soyuz program, on which the prestige of the Soviet Union depended.
Additional Details: New heavy-lift vehicle. References: 367.
1974 August 1 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. -
SSTTP M2-46 Target mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1974 August 6 - 00:02 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. -
Cosmos 670 Nation: USSR. Program: Salyut. Payload: Soyuz 7K-S s/n 1L. Mass: 6,700 kg (14,700 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-S. Agency: MOM. Perigee: 211 km (131 mi). Apogee: 294 km (182 mi). Inclination: 50.60 deg. Period: 89.50 min. COSPAR: 1974-061A. USAF Sat Cat: 7405. Duration: 2.99 days. Decay Date: 1974-08-09. Unmanned Soyuz 7K-S test flight. Recovered August 8, 1974 23:59 GMT. References: 2, 6, 21, 121.
1974 August 7 - 12:50 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 671 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 168 km (104 mi). Apogee: 304 km (188 mi). Inclination: 62.80 deg. Period: 89.20 min. COSPAR: 1974-062A. USAF Sat Cat: 7409. Duration: 13.00 days. Decay Date: 1974-08-20. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1974 August 8 - -
X-24 Flight 42 Nation: USA. Payload: X-24B flight 14. Class: Manned. Type: Spaceplane. Spacecraft: X-24B. Crew: Love Michael. Maximum Speed - 1644 kph. Maximum Altitude - 22370 m. Flight Time - 395 sec. References: 49, 97.
1974 August 9 - 03:22 GMT - Launch Site: Vandenberg. Launch Complex: SLC10W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Burner 2A. LV Configuration: Thor Burner 2A 275. -
DMSP-Block-5C F1 Nation: USA. Program: DMSP. Payload: DMSP 9532. Mass: 195 kg (429 lb). Class: Earth. Type: Weather. Spacecraft: DMSP Block 5C. Agency: USAF. Perigee: 779 km (484 mi). Apogee: 844 km (524 mi). Inclination: 98.80 deg. Period: 101.10 min. COSPAR: 1974-063A. USAF Sat Cat: 7411. Defense Meteorological Satellite Program. References: 2, 6.
1974 August 9 - 15:13 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3T. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1974 August 12 - 06:25 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. -
Cosmos 672 Nation: USSR. Program: ASTP. Payload: Soyuz ASTP s/n 72-EPSA. Mass: 6,570 kg (14,480 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-TM. Agency: MOM. Perigee: 222 km (137 mi). Apogee: 226 km (140 mi). Inclination: 51.70 deg. Period: 88.90 min. COSPAR: 1974-064A. USAF Sat Cat: 7413. Duration: 5.94 days. Decay Date: 1974-08-18. ASTP precursor. Recovered August 18, 1974 5:02 GMT. Soyuz ASTP test. Maneuver Summary: 195km X 305km orbit to 195km X 221km orbit. Delta V: 24 m/s 195km X 221km orbit to 223km X 223km orbit. Delta V: 8 m/s 231km X 231km orbit to 231km X 231km orbit. Delta V: 1 m/s 223km X 223km orbit to 231km X 231km orbit. Delta V: 4 m/s 231km X 231km orbit to 227km X 237km orbit. Delta V: 2 m/s Total Delta V: 39 m/s. Officially: Investigation of the upper atmosphere and outer space.
References: 2, 6.
1974 August 13 - Launch Vehicle: RLA. -
Glushko briefed his new RLA launch vehicle family to the VPK Military Industrial Commission Nation: USSR. These RLA - Rocket Flight Apparatus - met the requirements of the Ministry of Defence as described in 1973 in Plan Poisk and would replace the failed N1 and all existing launch vehicles. As required by the Ministry of Defence, they used only Lox/Kerosene propellants; the various launch vehicles were modular, and used common engines and rocket bodies. The members of the VPK met the proposal with considerable scepticism. The final decision was that the plan had to be reworked.
Additional Details: Glushko briefed his new RLA launch vehicle family to the VPK Military Industrial Commission. References: 367.
1974 August 13 - Launch Vehicle: Energia, N1. -
N1 work cancelled Nation: USSR. Program: Lunar L3. Spacecraft: LK, Soyuz 7K-LOK, Buran. Glushko formally cancelled the N1 within the new NPO Energia on 13 August 1974 with the support of Ustinov, even though he had no decree of the VPK Military-Industrial Commission or the Central Committee authorising such an act. The N1-L3 itself was not officially closed down until the resolution of February 1976 starting work on the Energia/Buran boosters. By that time 6 billion roubles had been spent on the N1 over 17 years.
Additional Details: N1 work cancelled. References: 367.
1974 August 14 - Launch Vehicle: N1. -
Glushko meets with TsKBEM staff Nation: USSR. Program: Lunar L3. Spacecraft: LK, Soyuz 7K-LOK. He solicited their support in the reorganization and new projects for the bureau. Glushko was sartorially perfect, and had an aristocratic air, never using the familiar forms of address in Russian. He only loosened up a little in the last years of his life. He was a nitpicker, correcting Russian syntax in documents. He was capable of clear logic but did not have the intuitive genius of Korolev (according to Barmin, while Korolev did not look after his appearance, he possessed a pure 'Russian' intelligence).
References: 367.
1974 August 14 - 15:45 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 24B. LV Configuration: Titan 24B 24B-12 (3B-46). -
OPS 3004 Nation: USA. Payload: KH-8 no. 43 / Agena D. Mass: 3,000 kg (6,600 lb). Class: Surveillance. Type: Military. Spacecraft: KH-8. Agency: NRO/USAF. Perigee: 135 km (83 mi). Apogee: 402 km (249 mi). Inclination: 110.50 deg. Period: 89.90 min. COSPAR: 1974-065A. USAF Sat Cat: 7416. Decay Date: 1974-09-29. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1974 August 14 - 18:08 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.417UA. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 133 km (82 mi). References: 2.
1974 August 16 - 03:41 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M. -
Cosmos 673 Nation: USSR. Program: Tselina. Payload: Tselina-D no. 6. Mass: 3,800 kg (8,300 lb). Class: Sigint. Spacecraft: Tselina-D. Agency: MOM. Perigee: 399 km (247 mi). Apogee: 416 km (258 mi). Inclination: 81.20 deg. Period: 92.70 min. COSPAR: 1974-066A. USAF Sat Cat: 7417. Decay Date: 1991-06-01. References: 2, 6.
1974 August 17 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 3. -
FOT GT45GM Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1974 August 17 - 05:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Ute Tomahawk. LV Configuration: Ute Tomahawk CRL A09.214-2. -
Vehicle Potential test Nation: USA. Agency: USAF CRL. Apogee: 161 km (100 mi). References: 2.
1974 August 18 - 08:59 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. -
Ferdinand 36 Ionosphere mission Nation: Norway. Agency: NDRE. Apogee: 106 km (65 mi). References: 2.
1974 August 19 - Launch Site: Baikonur. Launch Complex: LC105. Launch Pad: -. Launch Vehicle: R-36M. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1974 August 20 - 09:55 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-210. LV Configuration: S-210-10. -
NNP / NEL / TEL Aeronomy / ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 112 km (69 mi). References: 2.
1974 August 20 - 11:09 GMT - Launch Site: Grand Turk Island DZ. Launch Complex: -. Launch Pad: Aircraft from Cape Canaveral. Launch Vehicle: SRAM. FAILURE: Failure. -
Test mission Nation: USA. Agency: USAF. Apogee: 10 km (6 mi). References: 2.
1974 August 26 - -
Shuttle Enterprise fuselage assembly starts. Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise. Start structural assembly aft fuselage, Enterprise (OV-101) References: 15.
1974 August 26 - 19:58 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511. -
Soyuz 15 Nation: USSR. Program: Almaz. Payload: Soyuz 7K-T(A9) s/n 63. Mass: 6,760 kg (14,900 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-T/A9. Agency: MOM. Perigee: 173 km (107 mi). Apogee: 236 km (146 mi). Inclination: 51.60 deg. Period: 88.50 min. COSPAR: 1974-067A. USAF Sat Cat: 7421. Duration: 2.01 days. Decay Date: 1974-08-28. Crew: Demin, Sarafanov. Flight: Soyuz 15. Soyuz 15 was to conduct the second phase of manned operations aboard the Salyut 3 military space station, but the Igla rendezvous system failed and no docking was made. The two day flight could only be characterised as '... research in manoeuvring and docking with the OPS in various modes, and development of methods for evacuation and landing from space complex in new conditions....' As Chelomei had complained, Soyuz had no reserves or backup systems for repeated manual docking attempts and had to be recovered after a two-day flight. The state commission found that the Igla docking system of the Soyuz needed serious modification. This could not be completed before Salyut 3 decayed. Therefore the planned Soyuz 16 spacecraft became excess to the program (it was later flown as Soyuz 20 to a civilian Salyut station, even though over its two year rated storage life). Officially: Conduct of joint experiments with the Salyut-3 orbital scientific station.
References: 2, 6, 32, 33,60.
1974 August 27 - 14:59 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3T. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1974 August 28 - 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.
1974 August 28 - -
Landing of Soyuz 15 Nation: USSR. Program: Almaz. Flight: Soyuz 15. Soyuz 15 landed at 20:10 GMT.
1974 August 29 - -
X-24 Flight 43 Nation: USA. Payload: X-24B flight 15. Class: Manned. Type: Spaceplane. Spacecraft: X-24B. Crew: Manke. Maximum Speed - 1170 kph. Maximum Altitude - 22080 m. Flight Time - 467 sec. References: 49, 97.
1974 August 29 - 07:39 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 674 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 175 km (108 mi). Apogee: 323 km (200 mi). Inclination: 65.00 deg. Period: 89.50 min. COSPAR: 1974-068A. USAF Sat Cat: 7423. Duration: 9.00 days. Decay Date: 1974-09-07. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1974 August 29 - 14:55 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53719-154. -
Cosmos 675 Nation: USSR. Mass: 600 kg (1,320 lb). Spacecraft: Sfera. Agency: MO SSSR. Perigee: 1,364 km (847 mi). Apogee: 1,424 km (884 mi). Inclination: 74.10 deg. Period: 113.60 min. COSPAR: 1974-069A. USAF Sat Cat: 7424. Investigation of the upper atmosphere and outer space. References: 2, 6.
1974 August 30 - 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.
1974 August 30 - Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. FAILURE: Failure. -
Zenit-2M Nation: USSR. Payload: Zenit-2M. Spacecraft: Zenit-2M. Agency: RVSN. COSPAR: F740830A. Area survey photo reconnaissance satellite. References: 279.
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Nauka Nation: USSR. Payload: FEU-170 No. 3L. Spacecraft: Nauka. Agency: RVSN. COSPAR: F740830B. References: 279.
1974 August 30 - 14:07 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout D-1. LV Configuration: Scout D-1 S189C. FAILURE: Partial Failure. -
ANS 1 Nation: Netherlands. Mass: 129 kg (284 lb). Class: Astronomy. Spacecraft: ANS. Agency: NIVR. Perigee: 258 km (160 mi). Apogee: 1,173 km (728 mi). Inclination: 98.00 deg. Period: 99.10 min. COSPAR: 1974-070A. USAF Sat Cat: 7427. Decay Date: 1977-06-14. Astronomical Netherlands Satellite; lower than planned orbit. References: 2, 6.
1974 August 31 - Launch Vehicle: Energia, RLA. -
Competitive bidding for new vehicle Nation: USSR. Glushko proposed obtaining competitive bids for the launch complexes and booster subsystems for new boosters developed by OKB-1, dropping the traditional OKB-1 subcontractors. References: 367.
1974 August 31 - -
Cosmonaut reunion as Soyuz 15 crew arrives in Moscow. Nation: USSR. Program: Salyut. Flight: Soyuz 15. Kamanin attends a reunion of cosmonauts on the occasion of the arrival of the Soyuz 15 crew at Chkalovsky Airfield. Demin has flown at the age of 48, the oldest astronaut ever, until Slayton makes his flight. Kamanin talks to Glushko and learns that the N1 has finally been cancelled. The misbegotten project went for eight years only because of the unconditional support of Mishin by Keldysh, Smirnov, and Ustinov. The earliest Soviet lunar landing cannot occur earlier than the Tenth Five Year Plan (e.g. 1980). Kamanin learns that Soyuz 15 was supposed to be a thirty-day flight, but the Igla automatic docking system failed yet again.
References: 376.
1974 September 1 - Launch Site: Nenoksa. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-29. Model: Vysota. -
Test mission Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). References: 2.
1974 September 1 - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: -. Launch Vehicle: Lambda. Model: Lambda 4SC. LV Configuration: Lambda 4SC L-4SC-3. -
TVC test Nation: Japan. Agency: ISAS. Apogee: 1,500 km (900 mi). References: 2.
1974 September 2 - 06:00 GMT - Launch Site: Tanegashima. Launch Complex: Q. Launch Pad: -. Launch Vehicle: Mu. Model: ETV. LV Configuration: ETV-1. -
Test mission Nation: Japan. Agency: NASDA. Apogee: 128 km (79 mi). References: 2.
1974 September 3 - 23:25 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P99H. -
Plasmapause flux Ionosphere mission Nation: UK. Agency: SRC. Apogee: 136 km (84 mi). References: 2.
1974 September 4 - 10:24 GMT - Launch Site: Woomera. Launch Complex: LA8. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200. LV Configuration: Aerobee 200 CRL A05.391-1. -
HISTAR 8 Infrared astronomy mission Nation: USA. Agency: AFCRL. Apogee: 193 km (119 mi). References: 2.
1974 September 5 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. FAILURE: Failure. -
Combat training launch Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1974 September 6 - 23:59 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P94H. -
Plasmapause flux Ionosphere mission Nation: UK. Agency: SRC. Apogee: 174 km (108 mi). References: 2.
1974 September 7 - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.25DG. -
Astronomy mission Nation: USA. Agency: NASA. Apogee: 250 km (150 mi). References: 2.
1974 September 8 - Launch Site: Vandenberg. Launch Complex: 576A1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 80F. -
BMRS ACE-3 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi). References: 2.
1974 September 10 - Launch Site: Baikonur. Launch Complex: LC106. Launch Pad: -. Launch Vehicle: R-36M. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1974 September 11 - 11:02 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P90T/C. -
Mass spectrometer Atmospheric mission Nation: UK. Agency: SRC. Apogee: 135 km (83 mi). References: 2.
1974 September 11 - 17:40 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53719-151. -
Cosmos 676 Nation: USSR. Program: Strela. Mass: 750 kg (1,650 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-2M. Agency: MO SSSR. Perigee: 779 km (484 mi). Apogee: 798 km (495 mi). Inclination: 74.00 deg. Period: 100.60 min. COSPAR: 1974-071A. USAF Sat Cat: 7433. References: 2, 6.
1974 September 11 - 22:55 GMT - Launch Site: Woomera. Launch Complex: LA8. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200. LV Configuration: Aerobee 200 CRL A05.391-2. -
HISTAR 9 Infrared astronomy mission Nation: USA. Agency: AFCRL. Apogee: 200 km (120 mi). References: 2.
1974 September 12 - Launch Site: Kourou. Launch Complex: ALFS. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure 2C. LV Configuration: Centaure 2C (ESRO) C99/2. -
NO-II-2 Aeronomy mission Nation: Belgium. Agency: CNES. Apogee: 140 km (80 mi). References: 2.
1974 September 12 - Launch Site: Kourou. Launch Complex: ALFS. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure 2C. LV Configuration: Centaure 2C (ESRO) C99/1. -
NO-II-1 Aeronomy mission Nation: Belgium. Agency: CNES. Apogee: 140 km (80 mi). References: 2.
1974 September 13 - Launch Site: Kourou. Launch Complex: ALFS. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure 2C. LV Configuration: Centaure 2C (ESRO) C99/3. -
NO-II-3 Aeronomy mission Nation: Belgium. Agency: CNES. Apogee: 140 km (80 mi). References: 2.
1974 September 14 - -
Charles Kowal's Discovery of Jupiter Moon Leda Nation: USA.
1974 September 14 - 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.
1974 September 16 - 15:40 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-46. -
Plasma gun M / D Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 336 km (208 mi). References: 2.
1974 September 17 - 15:33 GMT - Launch Site: Woomera. Launch Complex: LA8. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200. LV Configuration: Aerobee 200 CRL A05.391-3. -
HISTAR Infrared astronomy mission Nation: USA. Agency: AFCRL. Apogee: 193 km (119 mi). References: 2.
1974 September 18 - 17:43 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.35US. -
Solar mission Nation: USA. Agency: NASA. Apogee: 252 km (156 mi). References: 2.
1974 September 19 - 02:00 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-47. -
Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 328 km (203 mi). References: 2.
1974 September 19 - 14:26 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Solar Ultraviolet/Solar Extreme ultraviolet mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 19 - 14:57 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53753-206. -
Cosmos 677 Nation: USSR. Program: Strela. Payload: Strela-1M no. 73. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,397 km (868 mi). Apogee: 1,466 km (910 mi). Inclination: 74.00 deg. Period: 114.50 min. COSPAR: 1974-072A. USAF Sat Cat: 7435. Eight satellites launched by a single carrier rocket. References: 2, 6.
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Cosmos 678 Nation: USSR. Program: Strela. Payload: Strela-1M no. 74. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,466 km (910 mi). Apogee: 1,532 km (951 mi). Inclination: 74.00 deg. Period: 116.00 min. COSPAR: 1974-072B. USAF Sat Cat: 7436. References: 2, 6.
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Cosmos 679 Nation: USSR. Program: Strela. Payload: Strela-1M no. 75. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,466 km (910 mi). Apogee: 1,511 km (938 mi). Inclination: 74.00 deg. Period: 115.70 min. COSPAR: 1974-072C. USAF Sat Cat: 7437. References: 2, 6.
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Cosmos 680 Nation: USSR. Program: Strela. Payload: Strela-1M no. 76. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,466 km (910 mi). Apogee: 1,492 km (927 mi). Inclination: 74.00 deg. Period: 115.50 min. COSPAR: 1974-072D. USAF Sat Cat: 7438. References: 2, 6.
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Cosmos 681 Nation: USSR. Program: Strela. Payload: Strela-1M no. 77. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,465 km (910 mi). Apogee: 1,472 km (914 mi). Inclination: 74.00 deg. Period: 115.30 min. COSPAR: 1974-072E. USAF Sat Cat: 7439. References: 2, 6.
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Cosmos 682 Nation: USSR. Program: Strela. Payload: Strela-1M no. 78. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,452 km (902 mi). Apogee: 1,467 km (911 mi). Inclination: 74.00 deg. Period: 115.10 min. COSPAR: 1974-072F. USAF Sat Cat: 7440. References: 2, 6.
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Cosmos 683 Nation: USSR. Program: Strela. Payload: Strela-1M no. 79. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,434 km (891 mi). Apogee: 1,466 km (910 mi). Inclination: 74.00 deg. Period: 114.90 min. COSPAR: 1974-072G. USAF Sat Cat: 7441. References: 2, 6.
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Cosmos 684 Nation: USSR. Program: Strela. Payload: Strela-1M no. 80. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,416 km (879 mi). Apogee: 1,466 km (910 mi). Inclination: 74.00 deg. Period: 114.70 min. COSPAR: 1974-072H. USAF Sat Cat: 7442. References: 2, 6.
1974 September 19 - 15:47 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 19 - 17:31 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 19 - 19:00 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 20 - Launch Site: Kwajalein. Launch Complex: Meck. Launch Pad: -. Launch Vehicle: Spartan. LV Configuration: Spartan ABM PFT-02A. -
Safeguard M2-245A Interceptor mission Nation: USA. Agency: USA. Apogee: 100 km (60 mi). References: 2.
1974 September 20 - 04:00 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 20 - 06:00 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 20 - 07:18 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 20 - 09:30 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 685 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 209 km (129 mi). Apogee: 281 km (174 mi). Inclination: 64.90 deg. Period: 89.30 min. COSPAR: 1974-073A. USAF Sat Cat: 7445. Duration: 12.00 days. Decay Date: 1974-10-02. Area survey photo reconnaissance satellite; returned film capsule. References: 2, 6.
1974 September 20 - 10:00 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 20 - 11:00 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 20 - 11:32 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-48. -
Precipitate Electrons Ionosphere / x-ray / ultraviolet mission Nation: Japan. Agency: ISAS. Apogee: 348 km (216 mi). References: 2.
1974 September 20 - 13:30 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 20 - 19:36 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 20 - 22:20 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 20 - 22:36 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 21 - -
Mariner 10 second flyby of Mercury Nation: USA. Spacecraft: Mariner 10. The second Mercury rendezvous provided another opportunity to photograph the sunlit side of the planet and the south polar region.
1974 September 21 - -
Mariner 10, second Mercury Flyby Nation: USA. Spacecraft: Mariner 10.
1974 September 21 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: Pioner. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi). References: 2.
1974 September 21 - 03:10 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Solar Ultraviolet/Solar Extreme ultraviolet mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 21 - 06:00 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1974 September 24 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Ute. Model: Nike Malemute. LV Configuration: Nike Malemute NASA 28.002GT. -
Test mission Nation: USA. Agency: NASA. Apogee: 465 km (288 mi). References: 2.
1974 September 24 - 23:17 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P50H. -
Airglow Atmospheric mission Nation: UK. Agency: SRC. Apogee: 136 km (84 mi). References: 2.
1974 September 26 - 16:34 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 686 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 72. Mass: 400 kg (880 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 279 km (173 mi). Apogee: 476 km (295 mi). Inclination: 70.90 deg. Period: 92.10 min. COSPAR: 1974-074A. USAF Sat Cat: 7447. Completed Operations Date: 1975-05-02. Decay Date: 1975-05-01. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1974 September 27 - 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.
1974 September 27 - 02:09 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P57H. -
Airglow Atmospheric mission Nation: UK. Agency: SRC. Apogee: 136 km (84 mi). References: 2.
1974 September 28 - 11:32 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P161H. -
Electron density Ionosphere mission Nation: UK. Agency: SRC. Apogee: 119 km (73 mi). References: 2.
1974 September 28 - 15:34 GMT - Launch Site: Vandenberg. Launch Complex: LF22. Launch Pad: -. Launch Vehicle: Minuteman 3. -
FOT GT46GB Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
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