Chronology - Quarter 4 1970 home
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1970 October 1 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Sandhawk Tomahawk. LV Configuration: Sandhawk Tomahawk Sandia 152-134.
  • Dualhawk-9 test Nation: USA. Agency: Sandia. Apogee: 515 km (320 mi). References: 2.
October 1970 - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -.
  • LC-1 at Baikonur refurbished Nation: USSR. In 1969 - 1970 LC-1 was refurbished. The refurbished complex could accommodate new versions of the Soyuz launch vehicle designed for Zenit reconnaisance satellites. The work was completed in October 1970. During the refurbishment a fire at the -32 m level in the flame pit killed four soldiers. The accident was apparently due to smoking of cigarettes in a corridor with an oxygen-rich atmosphere during liquid oxygen handling.
1970 October 1 - 08:20 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 366 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 216 km (134 mi). Apogee: 284 km (176 mi). Inclination: 65.00 deg. Period: 89.50 min. COSPAR: 1970-078A. USAF Sat Cat: 4561. Duration: 12.00 days. Decay Date: 1970-10-13. Area survey photo reconnaissance satellite; returned film capsule. References: 2, 6.
1970 October 1 - 13:46 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache N-NA-30.
  • DLR N-NA-30 Ionosphere / plasma mission Nation: Germany. Agency: DLR. Apogee: 200 km (120 mi). References: 2.
1970 October 3 -
  • DOS issues reviewed by VVS. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Kamanin meets with the General Staff to discuss issues with the DOS trainer. The issue of forming crews for the DOS program consisting only of unflown cosmonauts is debated. References: 376.
1970 October 3 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT46M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 October 3 - Launch Site: Kwajalein. Launch Complex: Meck. Launch Pad: -. Launch Vehicle: Spartan.
  • Safeguard M1-27 Interceptor mission Nation: USA. Agency: USA. Apogee: 100 km (60 mi). References: 2.
1970 October 3 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • SSTTP M1-27 Target mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1970 October 3 - 04:20 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5V.
  • RAO K-2 Solar x-ray mission Nation: USSR. Agency: AN SSSR. Apogee: 500 km (310 mi). References: 2.
1970 October 3 - 10:26 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
  • Cosmos 367 Nation: USSR. Program: RORSAT. Mass: 3,800 kg (8,300 lb). Class: Surveillance. Type: Naval Radarsat. Spacecraft: US-A. Agency: PKO. Perigee: 915 km (568 mi). Apogee: 1,022 km (635 mi). Inclination: 65.30 deg. Period: 104.50 min. COSPAR: 1970-079C. USAF Sat Cat: 4566. Decay Date: 1970-10-31. Ocean surveillance; probably used chemical batteries. References: 2, 6, 290.
1970 October 5 - 09:05 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.58IE.
  • MPE Barium release? Plasma mission Nation: USA. Agency: NASA. Apogee: 900 km (550 mi). References: 2.
1970 October 5 - 23:00 GMT - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • FOT GT77B Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 October 6 -
  • Cosmonaut training centre status. Nation: USSR. Program: Salyut, Almaz, Lunar L3. Spacecraft: Spiral OS, Almaz OPS. Kamanin reviews the work of the training centre in 1970-1971. There are 12 cosmonauts training for DOS missions; 22 for Almaz; 5 for Spiral; and a 'group' for the L3. They have flown 5000 flight hours in jet trainers. During the last two years Kamanin has increased the number of trainers and simulators available; achieved 100% of the training plan; and met the physical training requirements (all cosmonauts must accomplish a 10 km run). References: 376.
1970 October 6 -
  • Spiral spaceplane project review. Nation: USSR. Spacecraft: Spiral OS. Meeting with the Spiral spaceplane cosmonaut training group. Mikoyan and Dementiev (son of the MAP Minister) have been working on this project for four years. Many in the leadership (Grechko, Zakharov, Krylov, etc) are against the concept and hinder the project in any way the can. Grechko considers it 'a fantasy' and Kutakhov does not support it energetically. Engineer-Colonel Sokolov-Sokolenik is the head of the unit (having replaced Titov, who is now in staff school). The United States has hundreds of flights on the X-15, which they have taken to 90 km altitude and 7000 km/hour airspeed. In the Soviet Union, all such work has been frozen for a decade. References: 376.
1970 October 6 - 10:50 GMT - Launch Site: Biscarosse. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 3. LV Configuration: Dragon 3 D-305.
  • EIDI-1 Ionosphere mission Nation: France. Agency: CNES. Apogee: 480 km (290 mi). References: 2.
1970 October 6 - 13:36 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache N-NA-31.
  • DLR N-NA-31 Ionosphere / plasma mission Nation: Germany. Agency: DLR. Apogee: 200 km (120 mi). References: 2.
1970 October 6 - 15:15 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3P-5.
  • PEM-5 operational test launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1970 October 7 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT47M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 October 7 - 09:48 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.54NE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1970 October 8 -
  • President Pompidou of France visits Baikonur Nation: USSR. Pompidou visited Baikonur and was shown Bion and other open projects. This was in marked contrast to the exhibit provided to De Gaulle in 1966.
1970 October 8 - Launch Site: Baikonur. Launch Complex: LC142/34. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • Palma-4 Operational test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1970 October 8 - 08:20 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 6. LV Configuration: Skylark 6 SL972.
  • X-ray survey X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 232 km (144 mi). References: 2.
1970 October 8 - 12:39 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 368 Nation: USSR. Payload: Bion precursor. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 202 km (125 mi). Apogee: 383 km (237 mi). Inclination: 65.00 deg. Period: 90.40 min. COSPAR: 1970-080A. USAF Sat Cat: 4571. Duration: 6.00 days. Decay Date: 1970-10-14. Bion precursor mission. Conducted biological investigations and study of the physical characteristics of outer space. References: 2, 6.
1970 October 8 - 13:29 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache N-NA-32.
  • DLR N-NA-32 Ionosphere / plasma mission Nation: Germany. Agency: DLR. Apogee: 200 km (120 mi). References: 2.
1970 October 8 - 14:42 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache N-NA-33.
  • DLR N-NA-33 Ionosphere / plasma mission Nation: Germany. Agency: DLR. Apogee: 200 km (120 mi). References: 2.
1970 October 8 - 15:10 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
  • Cosmos 369 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 42. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 268 km (166 mi). Apogee: 509 km (316 mi). Inclination: 71.00 deg. Period: 92.30 min. COSPAR: 1970-081A. USAF Sat Cat: 4573. Completed Operations Date: 1971-01-22. Decay Date: 1971-01-22. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1970 October 9 - Launch Site: Wallops Island. Launch Complex: LA4. Launch Pad: -. Launch Vehicle: Sergeant. Model: Castor. LV Configuration: Castor-2R.
  • SPED II re-entry vehicle test flight Nation: USA. Agency: NASA. Apogee: 85 km (52 mi). References: 2.
1970 October 9 - 11:04 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 370 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 203 km (126 mi). Apogee: 280 km (170 mi). Inclination: 64.90 deg. Period: 89.30 min. COSPAR: 1970-082A. USAF Sat Cat: 4576. Duration: 13.00 days. Decay Date: 1970-10-22. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1970 October 12 - Launch Site: Baikonur. Launch Complex: LC161/35. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. FAILURE: Failure.
  • Palma-4 Operational test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1970 October 12 - 13:57 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: LC132/pad?. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M.
  • Cosmos 371 Nation: USSR. Mass: 775 kg (1,708 lb). Class: Navigation. Spacecraft: Tsiklon. Agency: MO SSSR. Perigee: 722 km (448 mi). Apogee: 728 km (452 mi). Inclination: 74.00 deg. Period: 99.30 min. COSPAR: 1970-083A. USAF Sat Cat: 4578. Military navigation satellite. References: 2, 6.
1970 October 12 - 14:58 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache N-NA-34.
  • DLR N-NA-34 Ionosphere / plasma mission Nation: Germany. Agency: DLR. Apogee: 200 km (120 mi). References: 2.
1970 October 13 - 00:08 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 SN5/2.
  • DLR S-CR-22 Aeronomy mission Nation: Germany. Agency: DFVLR. Apogee: 288 km (178 mi). References: 2.
1970 October 14 -
  • X-24 Flight 18 Nation: USA. Payload: X-24A flight 18. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Manke. First supersonic flight. Maximum Speed - 1261 kph. Maximum Altitude - 20696 m. Flight Time - 411 sec. References: 49, 97.
1970 October 14 -
  • Contacts on join USA/USSR docking system. Nation: USSR. Program: ASTP. Spacecraft: Soyuz 7K-TM. Communist Party Meeting at the cosmonaut centre. Keldysh calls later. Six specialists are to be sent to the United States to discuss design of a common USA/USSR docking system. Kamanin yet again goes through the correct answers and prepared speeches to be given to the press by Nikolayev and Sevastyanov on their visit to West Germany. References: 376.
1970 October 14 - 08:45 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 SL1021.
  • X-ray RMC X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 270 km (160 mi). References: 2.
1970 October 14 - 11:29 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/4. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
  • Intercosmos 4 Nation: USSR. Program: DS. Payload: DS-U3-IK s/n 2. Mass: 320 kg (700 lb). Class: Earth. Type: Magnetosphere. Spacecraft: DS-U3-IK. Agency: MO SSSR. Perigee: 255 km (158 mi). Apogee: 656 km (407 mi). Inclination: 48.40 deg. Period: 93.70 min. COSPAR: 1970-084A. USAF Sat Cat: 4580. Completed Operations Date: 1971-01-08. Decay Date: 1971-01-17. Investigation of the ultra-violet and x-radiation of the sun and its effect on the structure of the Earth's upper atmosphere. Payload included East European experiments to study solar ultraviolet and X-ray effects on upper atmosphere. References: 2, 6, 99, 116.
1970 October 14 - 16:41 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.276AM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 116 km (72 mi). References: 2.
1970 October 15 - 11:22 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
  • Meteor 1-06 Nation: USSR. Payload: Meteor M no. 6. Mass: 3,800 kg (8,300 lb). Class: Earth. Type: Weather. Spacecraft: Meteor M. Agency: MOM. Perigee: 441 km (274 mi). Apogee: 443 km (275 mi). Inclination: 81.20 deg. Period: 93.40 min. COSPAR: 1970-085A. USAF Sat Cat: 4583. Decay Date: 1999-01-08. Acquisition of meteorological information needed for use by the weather service. References: 2, 6.
1970 October 16 -
  • Mishin seems to have lost his fight for a water landing on L3 missions. Nation: USSR. Program: Lunar L3. Spacecraft: Soyuz 7K-LOK. All will have to be on dry land. 500 million roubles would have been necessary to fund the sea forces, and the risk to the crews would have been greater. Kamanin sees the whole bogus controversy as a diversionary tactic of Mishin's to take attention away from the fact that the L3 spacecraft is in fact nonexistent - as is its N1 rocket. An additional 300 million roubles are needed to achieve a 'flying' N1. A completely new solution to the lunar landing problem needs to be worked out. Shatalov worked today with Grechko to lay out the program for French President Pompidou's visit to the Baikonur cosmodrome. Pompidou wants to see two live rocket launches, and Shatalov will show him the Soyuz spacecraft. References: 376.
1970 October 16 - 00:30 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC S53. FAILURE: Failure.
  • ESRO S53 Solar x-ray mission Nation: UK. Agency: BAC/ESRO. Apogee: 209 km (129 mi). References: 2.
1970 October 16 - 14:59 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53717-04.
  • Cosmos 372 Nation: USSR. Program: Strela. Mass: 750 kg (1,650 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-2M. Agency: MO SSSR. Perigee: 767 km (476 mi). Apogee: 787 km (489 mi). Inclination: 74.10 deg. Period: 100.40 min. COSPAR: 1970-086A. USAF Sat Cat: 4588. References: 2, 6.
1970 October 19 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC S58. FAILURE: Failure.
  • ESRO S58 Solar ultraviolet mission Nation: UK. Agency: BAC/ESRO. Apogee: 200 km (120 mi). References: 2.
1970 October 20 - 05:38 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
  • Cosmos 373 Nation: USSR. Mass: 650 kg (1,430 lb). Class: Military. Type: ASAT Target. Spacecraft: IS-P. Agency: PKO. Perigee: 510 km (310 mi). Apogee: 1,103 km (685 mi). Inclination: 62.90 deg. Period: 101.00 min. COSPAR: 1970-087A. USAF Sat Cat: 4590. Decay Date: 1980-03-08. ASAT target. Maneuvered twice to provide target for Cosmos 374 and 375 interceptors. References: 2, 6, 272.
1970 October 20 - 13:05 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Ionosphere mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1970 October 20 - 19:55 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/D. LV Configuration: Proton-K/D 250-01.
  • Zond 8 Nation: USSR. Program: Lunar L1. Payload: Soyuz 7K-L1 s/n 14. Mass: 5,390 kg (11,880 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-L1 . Agency: MOM. Perigee: 200 km (120 mi). Apogee: 400,000 km (240,000 mi). Inclination: 51.60 deg. Period: 15,562.22 min. COSPAR: 1970-088A. USAF Sat Cat: 4591. Duration: 5.17 days. Decay Date: 1970-10-27. Final circumlunar flight; successfully recovered October 26, 1970. The announced objectives were investigations of the moon and circumlunar space and testing of onboard systems. The spacecraft obtained photographs of the earth on October 21 from a distance of 64,480 km. The spacecraft transmitted flight images of the earth for three days. Zond 8 flew past the moon on October 24, 1970, at a distance of 1,110.4 km and obtained both black and white and colour photographs of the lunar surface. Scientific measurements were also obtained during the flight. The spacecraft used a new variant of the double-dip re-entry, coming in over the north pole, bouncing off the atmosphere, being tracked by Soviet radar stations as it soared south over the Soviet Union, then making a final precision re-entry followed by splashdown at the recovery point in the Indian Ocean. References: 2, 6, 67, 274, 296.
1970 October 21 - 09:39 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Cockatoo. LV Configuration: Cockatoo 106.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi). References: 2.
1970 October 21 - 13:25 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Ionosphere mission Nation: USSR. Apogee: 176 km (109 mi). References: 2.
1970 October 21 - 14:30 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Plasma mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1970 October 21 - 15:03 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Ionosphere/Plasma mission Nation: USSR. Apogee: 168 km (104 mi). References: 2.
1970 October 22 - 08:23 GMT - Launch Site: Biscarosse. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 3. LV Configuration: Dragon 3 D-306.
  • EIDI-2 Ionosphere mission Nation: France. Agency: CNES. Apogee: 480 km (290 mi). References: 2.
1970 October 22 - 14:24 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache N-NA-35.
  • DLR N-NA-35 Ionosphere / plasma mission Nation: Germany. Agency: DLR. Apogee: 200 km (120 mi). References: 2.
1970 October 22 - 22:35 GMT - Launch Site: Vandenberg. Launch Complex: LF25. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT69F (Salvo) operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 October 22 - 22:35 GMT - Launch Site: Vandenberg. Launch Complex: LF26. Launch Pad: LF26?. Launch Vehicle: Minuteman 2.
  • OT GT70F (Salvo) operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 October 23 -
  • Mishin still fighting for an ocean landing for the L3. Nation: USSR. Program: Lunar L3. Spacecraft: Soyuz 7K-LOK. He has recruited some cosmonauts and admirals to fight for the concept. References: 376.
1970 October 23 - Launch Site: Baikonur. Launch Complex: LC162/36. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67P.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1970 October 23 - 04:42 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
  • Cosmos 374 Nation: USSR. Mass: 1,400 kg (3,000 lb). Class: Military. Type: ASAT. Spacecraft: IS-A. Agency: PKO. Perigee: 531 km (329 mi). Apogee: 1,464 km (909 mi). Inclination: 63.00 deg. Period: 105.10 min. COSPAR: 1970-089A. USAF Sat Cat: 4594. Decay Date: 1970-10-23. ASAT interceptor. Intercepted Cosmos 374 on second orbit. Blown up on instructions from ground. References: 2, 6, 272.
1970 October 23 - 17:40 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3B. LV Configuration: Titan 23B 23B-7 (3B-29).
  • OPS 7568 Nation: USA. Payload: KH-8 no. 29 / 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: 396 km (246 mi). Inclination: 111.10 deg. Period: 89.80 min. COSPAR: 1970-090A. USAF Sat Cat: 4596. Decay Date: 1970-11-11. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1970 October 23 - 22:00 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3E-5.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1970 October 24 -
  • Cosmonauts oppose ocean landing for the L3. Nation: USSR. Program: Lunar L3. Spacecraft: Soyuz 7K-LOK. 18 VVS officers and cosmonauts meet to discuss the L3 water landing issue. Kamanin is to draft a letter against the concept to Mishin and Afanaseyev. References: 376.
1970 October 26 -
  • Gagarin documentary. Nation: USSR. Leningrad Television is making a program about Gagarin. People are coming out of the woodwork that knew him or claimed to have known him. New facts are expected to emerge. References: 376.
1970 October 26 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • FOT GT78B Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 October 27 -
  • X-24 Flight 19 Nation: USA. Payload: X-24A flight 19. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Manke. Maximum Speed - 1446 kph. Maximum Altitude - 21763 m. Flight Time - 417 sec. References: 49, 97.
1970 October 27 - 20:34 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S67/1.
  • ESRO S67 / 1 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 229 km (142 mi). References: 2.
1970 October 28 -
  • Chelomei's 'war' with Korolev and Mishin Nation: USSR. Program: Almaz, Salyut, Lunar L1. Spacecraft: Almaz OPS, Salyut 1, LK-1, Soyuz 7K-L1. Kamanin meets with Chelomei. Chelomei discusses his 'war' with Korolev and Mishin. Korolev interfered with, and then finally took the manned lunar flyby project from Chelomei. Now Mishin is doing the same thing with Almaz. Chelomei had already invested five years in development of Almaz, and was on the way to producing a good space station. Then Mishin pushes him out of the way and seizes his production line to build the DOS-7K. DOS#1 is actually Almaz#5, nothing more than a bad copy of Chelomei's station. Serbin and Smirnov do not trust Mishin, which is why they have only authorised him to build four DOS stations. Serbin, Smirnov, and Afanasyev have visited Chelomei, and told him to accelerate work on the Almaz, using three shifts 24 hours a day.

    Kamanin notes the second hijacking in Turkey of a Soviet airliner in the last two weeks. References: 376.

1970 October 28 -
  • Cosmonauts learn of NASA techniques. Nation: USSR. Nikolayev and Sevastyanov return from their tour of the USA, They learned a lot about the technology, management, and training techniques of the American space program. Nikolayev leaves immediately for another tour of Czechoslovakia. References: 376.
1970 October 28 -
  • Zond 8 recovered, demonstrates Mishin's L3 ocean landing trajectory. Nation: USSR. Program: Lunar L1, Lunar L3. Spacecraft: Soyuz 7K-LOK, Soyuz 7K-L1. Zond 8 is recovered only 15 minutes after splashdown by the vessel Taman. Of five Zonds recovered, this was the only one to fly over the north pole. The remainder re-entered over the south pole. The reason for this was the need to fly over tracking stations on Soviet territory in order to get trajectory updates that allowed a precise landing after the second plunge into the atmosphere. This was the reason Mishin now wants a water landing for the L3. The dilemma is that after a first dip into the atmosphere over the North Pole, tracking for a precision landing is possible, but then the spacecraft cannot land on Soviet territory. Re-entering first over the South Pole means that no trajectory updates are available, but then the spacecraft can land only imprecisely somewhere on Soviet territory.

    15 L1's were completed, of which only five ever returned to earth. With this successful final recovery, the programme is cancelled. The main cause of the project's failure was the unreliability of the UR-500K rocket. References: 376.

1970 October 28 - Launch Site: Kwajalein. Launch Complex: Meck. Launch Pad: -. Launch Vehicle: Sprint. FAILURE: Failure.
  • Safeguard M1-9 Interceptor mission Nation: USA. Agency: USA. Apogee: 0 km ( mi). References: 2.
1970 October 28 - 16:23 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.131UA.
  • Structure Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1970 October 29 - Launch Site: Baikonur. Launch Complex: LC142/34. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1970 October 29 - 21:39 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S67/2.
  • ESRO S67 / 2 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 234 km (145 mi). References: 2.
1970 October 30 -
  • Shatalov and Yeliseyev selected for first space station flight. Nation: USSR. Program: Salyut. Flight: Soyuz 10. Shatalov and Yeliseyev are selected as the prime crew to man DOS#1. This selection is made even though they have both made two flights already and other cosmonauts have been waiting six years with no flight assignment. The choice is due to the role of the pilot, who it is felt must have prior docking experience. Kamanin reviews the training schedule for the pair, plus a tour of India they will have to make before the flight. References: 376.
1970 October 30 - 02:36 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
  • Cosmos 375 Nation: USSR. Mass: 1,400 kg (3,000 lb). Class: Military. Type: ASAT. Spacecraft: IS-A. Agency: PKO. Perigee: 579 km (359 mi). Apogee: 1,986 km (1,234 mi). Inclination: 62.80 deg. Period: 111.20 min. COSPAR: 1970-091A. USAF Sat Cat: 4598. Decay Date: 1970-10-30. ASAT interceptor. Intercept on second orbit. Blown up on instructions from ground. Dual launch of interceptors was intended to help ground staff perfect computational methods for quick-response launches when orbital methods of target were not precisely known. References: 2, 6, 272.
1970 October 30 - 13:20 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 376 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 207 km (128 mi). Apogee: 286 km (177 mi). Inclination: 65.40 deg. Period: 89.40 min. COSPAR: 1970-092A. USAF Sat Cat: 4599. Duration: 13.00 days. Decay Date: 1970-11-12. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1970 October 31 - Launch Vehicle: Proton. Model: Proton 8K82K. LV Configuration: Proton 8K82K.
  • Soyuz 7K-L1 s/n 10L and 15L Nation: USSR. Program: Lunar L1. Payload: Soyuz 7K-L1 s/n 10L and 15L. Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-L1. Despite decision to cancel immediate manned circumlunar flights after Apollo 8, the remaining two L-1 spacecraft were kept in reserve for support of the L3 lunar landing program and possible later manned flights. They were never used. References: 23.
1970 October 31 - 10:32 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.41GG-UG.
  • Astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1970 November 1 - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: RT-2.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1970 November 1 - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: RT-2.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1970 November 2 -
  • M2 Flight 19 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 3. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Dana. Maximum Speed - 690 kph. Maximum Altitude - 13716 m. Flight Time - 236 sec. References: 49, 97.
1970 November 2 - 23:05 GMT - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT51M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 November 4 - 09:05 GMT - Launch Site: Vandenberg. Launch Complex: LF21. Launch Pad: -. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-1W.
  • STM-1W research and development mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1970 November 5 - Launch Site: Baikonur. Launch Complex: LC162/36. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1970 November 6 - 02:00 GMT - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT52M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 November 6 - 03:36 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Cockatoo. LV Configuration: Cockatoo 108.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi). References: 2.
1970 November 6 - 10:35 GMT - Launch Site: Cape Canaveral. Launch Complex: LC40. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3C. LV Configuration: Titan IIIC 23C-1 (3C-19). FAILURE: Partial Failure.
  • IMEWS 1 Nation: USA. Payload: DSP Phase 1 s/n 1. Mass: 900 kg (1,980 lb). Class: Early Warning. Spacecraft: DSP. Agency: USAF. Perigee: 25,840 km (16,050 mi). Apogee: 36,128 km (22,448 mi). Inclination: 16.40 deg. Period: 1,197.90 min. COSPAR: 1970-093A. USAF Sat Cat: 4630. Completed Operations Date: 1973-12-31. First generation geosynchronous ballistic missile launch detection satellite; placed in incorrect subsynchronous orbit. One account claimed that it exhausted its propellant before it could be put into operation, but a 2007service history chart showed that is was considered operational for three years, well beyond its planned life. References: 2, 6, 127.
1970 November 8 - 07:50 GMT - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • FOT GT79B Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 November 9 -
  • Cosmonauts have perfect flight safety record since Gagarin's crash. Nation: USSR. The cosmonaut's Seregin Regiment has now flown 4500 hours without an accident. The safety record for the VVS was 18,000 hours between crashes in 1969, 22,000 in 1970 so far. References: 376.
1970 November 9 - 06:00 GMT - Launch Site: Wallops Island. Launch Complex: LA3A. Launch Pad: -. Launch Vehicle: Scout. Model: Scout B. LV Configuration: Scout B S174C.
  • OFO 1 Nation: USA. Payload: OFO 1 / RM 1. Mass: 133 kg (293 lb). Class: Biology. Spacecraft: OFO. Agency: NASA ARC. Perigee: 304 km (188 mi). Apogee: 518 km (321 mi). Inclination: 37.40 deg. Period: 92.60 min. COSPAR: 1970-094A. USAF Sat Cat: 4690. Decay Date: 1971-05-09. Orbiting Frog Otolith. The satellite carrying the OFO-A experiment remained in orbit for almost seven days. Recovery of the spacecraft was not planned. The payload was the Frog Otolith Experiment Package (FOEP). The objective of the experiment was to investigate the effect of microgravity on the otolith, a sensory organ that responds to changes in an animal's orientation within the Earth's gravitational field. Two bullfrogs (Rana catesbeiana) were used as experimental subjects in the flight experiment. Additional Details: OFO 1. References: 2, 6, 297.
  • RM-1; RMS Nation: USA. Payload: RM/FW4S. Mass: 46 kg (101 lb). Class: Earth. Type: Micrometeoroid. Spacecraft: RM. Agency: NASA MSC. Perigee: 303 km (188 mi). Apogee: 526 km (326 mi). Inclination: 37.40 deg. Period: 92.70 min. COSPAR: 1970-094B. USAF Sat Cat: 4692. Decay Date: 1971-02-07. Radiation Meteoroid. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1970 November 10 - Launch Site: Biscarosse. Launch Complex: BLB. Launch Pad: -. Launch Vehicle: SSBS. Model: SSBS S02. LV Configuration: SSBS S02 C6.
  • S02C6 test Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi). References: 2.
1970 November 10 - 11:09 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.92UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1970 November 10 - 14:44 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/D. LV Configuration: Proton-K/D 251-01.
  • Luna 17 Nation: USSR. Program: Luna. Payload: Ye-8 s/n 203. Mass: 5,600 kg (12,300 lb). Class: Planetary. Type: Lunar. Spacecraft: Luna Ye-8. Agency: MOM. Perigee: 85 km (52 mi). Apogee: 85 km (52 mi). Inclination: 141.00 deg. Period: 116.00 min. COSPAR: 1970-095A. USAF Sat Cat: 4691. Decay Date: 1970-11-17. Luna 17 was launched from an earth parking orbit towards the Moon and entered lunar orbit on November 15, 1970. Luna 17 landed on Moon 17 November 1970 at 03:47:00 GMT, Latitude 38.28 N, Longitude 325.00 E - Mare Imbrium (Sea of Rains). The payload, the Lunokhod 1 unmanned rover, rolled down a ramp from the landing stage and began exploring the surface. Lunokhod was intended to operate through three lunar days but actually operated for eleven lunar days (earth months). The operations of Lunokhod officially ceased on October 4, 1971, the anniversary of Sputnik 1. By then it had traveled 10,540 m and had transmitted more than 20,000 TV pictures and more than 200 TV panoramas. It had also conducted more than 500 lunar soil tests. Parameters are for lunar orbit. References: 2, 6, 67, 274, 296.
1970 November 11 - 04:55 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL905.
  • X-ray Survey X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 183 km (113 mi). References: 2.
1970 November 11 - 09:20 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 377 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 286 km (177 mi). Inclination: 65.00 deg. Period: 89.30 min. COSPAR: 1970-096A. USAF Sat Cat: 4695. Duration: 12.00 days. Decay Date: 1970-11-23. Area survey photo reconnaissance satellite; returned film capsule. References: 2, 6.
1970 November 12 - 11:00 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Cockatoo. LV Configuration: Cockatoo 105.
  • Lunar ultraviolet Ozone Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 104 km (64 mi). References: 2.
1970 November 13 - Launch Vehicle: Shuttle.
  • Shuttle specifications revised Nation: USA. Further minor changes were made as a result of the NASA 90-day review in October. References: 44.
1970 November 13 - 22:19 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.115IE.
  • Ferdinand 23 Auroral mission Nation: USA. Agency: NASA. Apogee: 214 km (132 mi). References: 2.
1970 November 14 - Launch Site: Vandenberg. Launch Complex: LF08. Launch Pad: -. Launch Vehicle: Minuteman 3.
  • OLD FOX 03M demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 November 16 -
  • Nikolayev-Tereshkova marital problems a VVS management issue Nation: USSR. Kamanin has a difficult and unpleasant conversation with Tereshkova. She and her mother have written to generals in the chain of command over Kamanin several times about Nikolayev's bad behaviour. This was never mentioned to Kamanin. He doesn't know what to do about the quarrels between the 'space couple'. References: 376.
1970 November 16 - 20:00 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P37H.
  • Particles Ionosphere mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1970 November 17 -
  • Indecision on DOS profile; Almaz station accelerated. Nation: USSR. Program: Almaz, Salyut. Spacecraft: Salyut 1, Almaz OPS. It is decided to send only Volynov and Khrunov to the FAI Congress in India. Shatalov and Yeliseyev are too busy with training on the DOS-7K simulator. Luna 17 has landed on the moon with the Lunokhod lunar rover, another success. DOS#1 is behind schedule for the planned 5 February 1971 launch. It still has not been decided, which will launch first - Soyuz 10 or the DOS station. Such indecision makes it very difficult to train the crews! The simulators for Soyuz, L3, DOS, and Almaz are all now in full use for crew training. Kamanin discusses with engineers construction of a pool for EVA training (25 m wide and 12 m deep). Kutakahov is opposed to the project. Chelomei has been ordered to accelerate the first Almaz launch to 1972, if he can resist the continuous attacks by Mishin. Mishin has become very accomplished, on the N1/L3 program, in spending huge amounts of money with no result. References: 376.
1970 November 17 - 18:20 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47117-107.
  • Cosmos 378 Nation: USSR. Program: DS. Payload: DS-U2-IP s/n 1. Mass: 710 kg (1,560 lb). Class: Earth. Type: Ionosphere. Spacecraft: DS-U2-IP. Agency: MO SSSR. Perigee: 234 km (145 mi). Apogee: 1,742 km (1,082 mi). Inclination: 74.00 deg. Period: 104.90 min. COSPAR: 1970-097A. USAF Sat Cat: 4713. Completed Operations Date: 1971-09-13. Decay Date: 1972-08-17. Studied the ionosphere and charged particle flows. References: 2, 6, 99.
1970 November 18 -
  • Luna 17 lands on moon. Nation: USSR. Program: Luna. Spacecraft: Luna Ye-8, Lunokhod. Luna 17 / Lunokhod have landed on the Sea of Storms on the moon. Chelomei is assisting Kamanin in securing funds for the water basin for zero-G training, further simulators, etc. References: 376.
1970 November 18 - 12:30 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.93UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1970 November 18 - 21:29 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Delta. Model: Thorad SLV-2H Agena D. LV Configuration: Thorad SLV-2H Agena D 552 / Agena D 1658.
  • KH-4B 1112 Nation: USA. Payload: KH-4B s/n 1112 / Agena D 1658. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4B. Agency: NRO/CIA. Perigee: 180 km (110 mi). Apogee: 227 km (141 mi). Inclination: 82.90 deg. Period: 88.50 min. COSPAR: 1970-098A. USAF Sat Cat: 4721. Decay Date: 1970-12-11. KH-4B. The forward camera failed on pass 104 and remained inoperative throughout the rest of the mission. References: 2, 6.
  • SRV 827 Nation: USA. Payload: SRV 1112-1. Mass: 60 kg (132 lb). Spacecraft: KH-4B. Agency: NRO/USAF. Perigee: 493 km (306 mi). Apogee: 505 km (313 mi). Inclination: 83.10 deg. Period: 94.60 min. COSPAR: 1970-098B. USAF Sat Cat: 4722. Decay Date: 1977-09-14. Radar monitoring. References: 2, 6, 172.
  • OPS 6829 Nation: USA. Payload: EHH B20. Class: Sigint. Spacecraft: SSF. Agency: USAF. COSPAR: 1970-098xx. USAF Sat Cat: 4722. Decay Date: 1977-09-14. References: 2, 279.
1970 November 19 - 06:16 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P47H.
  • VLF fields Ionosphere mission Nation: UK. Agency: SRC. Apogee: 129 km (80 mi). References: 2.
1970 November 19 - 22:00 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL904.
  • XRB anisotropy X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 209 km (129 mi). References: 2.
1970 November 20 -
  • X-24 Flight 20 Nation: USA. Payload: X-24A flight 20. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Gentry. Maximum Speed - 1456 kph. Maximum Altitude - 20604 m. Flight Time - 432 sec. References: 49, 97.
1970 November 20 - 19:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.458UA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1970 November 20 - 22:19 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.917-1.
  • Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 170 km (100 mi). References: 2.
1970 November 20 - 22:19 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.901-6.
  • Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 150 km (90 mi). References: 2.
1970 November 20 - 22:23 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AT07.895.
  • Mass spectrometer Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 121 km (75 mi). References: 2.
1970 November 20 - 22:23 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AT07.896.
  • Mass spectrometer Ionosphere mission Nation: USA. Agency: AFCRL. Apogee: 130 km (80 mi). References: 2.
1970 November 20 - 22:26 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.917-3.
  • Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 166 km (103 mi). References: 2.
1970 November 20 - 22:26 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.917-2.
  • Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 158 km (98 mi). References: 2.
1970 November 20 - 23:29 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.460UM.
  • UM Pitot 52 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 181 km (112 mi). References: 2.
1970 November 21 - 23:56 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trailblazer. Model: Trailblazer 2. LV Configuration: Trailblazer 2 CRL AD21.862.
  • AFCRL TB2-3 Re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 321 km (199 mi). References: 2.
1970 November 23 -
  • First lunar rover. Nation: USSR. Program: Luna. Spacecraft: Luna Ye-8, Lunokhod. Lunokhod 1 is ready to go on its first lunar drive. References: 376.
1970 November 24 -
  • DOS ECS delays. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. A gala is held at the Soviet Army Theater on the occasion of the 50th Anniversary of the Zhukovskiy Flight Academy. There is also a meeting of the Central Chess Club of the USSR to honour the first space-earth chess match played during the Soyuz 9 flight. Even Spasskiy is there. IMBP has advised the environmental control system for DOS#1 will not be ready in time to support a 5 February launch. References: 376.
1970 November 24 - 02:18 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Bullpup Apache.
  • Aeronomy / Barium release mission Nation: USA. Agency: NSF. Apogee: 50 km (31 mi). References: 2.
1970 November 24 - 05:15 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511L.
  • Cosmos 379 Nation: USSR. Program: Lunar L3. Payload: Lunar Craft T2K no. 1. Mass: 5,500 kg (12,100 lb). Class: Manned. Type: Lunar lander. Spacecraft: LK. Agency: MOM. Perigee: 198 km (123 mi). Apogee: 232 km (144 mi). Inclination: 51.60 deg. Period: 88.70 min. COSPAR: 1970-099A. USAF Sat Cat: 4760. Duration: 4,683.78 days. Decay Date: 1983-09-21. LK moon lander test using the T2K version. First use of the Soyuz 11A511L booster modified especially for this purpose. The spacecraft made a series of engine burns, simulating the lunar landing profile. After 3.5 days in orbit, the first burn was made in imitation of a descent to the lunar surface after separation of the Block D lunar crasher stage. The orbit changed from 192 km X 233 km to 196 km X 1206 km orbit; delta V: 263 m/s. After 4 days in orbit, a large manoeuvre was made simulating the ascent from the lunar surface. The orbit was changed from 188 km X 1198 km to 177 km X 14,041 km; delta V: 1518 m/s. These main manoeuvres were followed by a series of small adjustments simulating rendezvous and docking with the LOK. The LK tested out without major problems and decayed from orbit on September 21, 1983. References: 2, 6.
1970 November 24 - 10:59 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
  • Cosmos 380 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 26. Mass: 250 kg (550 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 199 km (123 mi). Apogee: 1,520 km (940 mi). Inclination: 82.00 deg. Period: 102.20 min. COSPAR: 1970-100A. USAF Sat Cat: 4762. Completed Operations Date: 1970-11-26. Decay Date: 1971-06-17. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1970 November 24 - 20:45 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.285CS.
  • Solar mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1970 November 24 - 22:13 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL804.
  • X-ray crystal spectrometer Solar x-ray mission Nation: UK. Agency: BAC. Apogee: 182 km (113 mi). References: 2.
1970 November 25 -
  • M2 Flight 20 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 4. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Dana. First powered flight. Maximum Speed - 859 kph. Maximum Altitude - 15819 m. Flight Time - 377 sec. References: 49, 97.
1970 November 25 -
  • NASA Administrator discussed significance of Russian unmanned lunar probes to Apollo. Nation: USA. Program: Apollo. Spacecraft: Luna Ye-8, Lunokhod. George M. Low, Acting NASA Administrator, discussed the significance of unmanned lunar probes Luna XVI and XVII launched by the U.S.S.R. September 12 and November 10. Luna XVI had brought lunar samples back to earth and Luna XVII had landed an unmanned Lunokhod roving vehicle on the moon's surface. Low stated in a letter to Chairman Clinton P. Anderson of the Senate Committee on Aeronautical and Space Sciences that while the two launches were impressive their contributions to science and technology were relatively minor. Low suggested that the main lesson to be learned from the two launches specifically and the U.S. and U.S.S.R. space programs in general was that while the Soviet launch rate was increasing that of the United States was decreasing. These trends in the two countries' space programs should be a cause of concern if the United States was interested in maintaining a position of leadership in space. References: 16.
1970 November 25 -
  • TsPK Deputy Commander appointment disputed. Nation: USSR. Kamanin is being pressured to replace the Deputy Commander of the training centre with a non-cosmonaut officer. References: 376.
1970 November 25 - 03:17 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Scout. Model: Blue Scout Jr SLV-1C. LV Configuration: Blue Scout Jr SLV-1C NB22.208.
  • Ultraviolet Telescope Ultraviolet astronomy mission Nation: USA. Agency: USN. Apogee: 1,480 km (910 mi). References: 2.
1970 November 26 -
  • Kutakhov opposes expanded VVS role in space. Nation: USSR. Spacecraft: Spiral OS. Kutakhov visits the cosmonaut training centre. He is still against the VVS being involved in manned spaceflight. He tells Kamanin that Kamanin's draft resolution on the use of space for reconnaissance, communications, navigation, and piloted flight is not appropriate for 1971 - more like 1980. In the evening, Kamanin talks to Nikolayev about Tereshkova's complaints. He claims that in seven years he has only had two or three of these blow-ups with her. He blames her in-laws for starting the whole thing and keeping the bad feelings going. References: 376.
1970 November 27 -
  • VVS considers role in space. Nation: USSR. Program: Almaz. Spacecraft: Spiral OS, Almaz OPS. The leaders of the VVS meet to consider the role of the Air Force in space and Kamanin's draft resolution. Frolov wants to form a VVS regiment for Almaz operations. Molzhavtsev wants to emphasize full use of unmanned satellites for support of the VVS (communications, navigation, reconnaissance). Later in the meeting V V Kuznestov discusses with Kamanin plans for a planned Nikolayev-Tereshkova-Sevastyanov trip to Egypt in January 1971. It has to be planned around opening ceremonies for the Aswan Dam. References: 376.
1970 November 27 - 15:47 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M.
  • Molniya 1-16 Nation: USSR. Program: Molniya. Payload: Molniya-1. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-1. Agency: MOM. Perigee: 463 km (287 mi). Apogee: 39,895 km (24,789 mi). Inclination: 65.50 deg. Period: 717.80 min. COSPAR: 1970-101A. USAF Sat Cat: 4779. Decay Date: 1975-11-25. Operation of a system of long range telephone-telegraph radiocommunication, and transmission of USSR Central Television programmes to the stations of the Orbita network. References: 2, 6, 64.
1970 November 27 - 20:15 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Apogee: 160 km (90 mi). References: 2.
1970 November 27 - 22:17 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3E-10.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1970 November 28 - 05:30 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5V.
  • Vertikal-1 Aeronomy / ionosphere / solar mission Nation: USSR. Agency: AN SSSR. Apogee: 468 km (290 mi). References: 2.
1970 November 30 - 22:40 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36B. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3C Centaur. LV Configuration: SLV-3C Centaur AC-21 / Centaur D-1A 5003C. FAILURE: Shroud failed to separate.
  • OAO-B Nation: USA. Payload: OAO B. Mass: 2,121 kg (4,676 lb). Class: Astronomy. Spacecraft: OAO. Agency: NASA. COSPAR: F701130A. Decay Date: 1970-11-30. Orbiting Astronomical Observatory. Launch vehicle was to have put payload into geosynchronous transfer orbit References: 126, 278.
1970 December 1 - Launch Vehicle: Shuttle.
  • Shuttle Phase B preliminary proposals Nation: USA. The teams of McDonnell Douglas/Martin Marrietta and North American Rockwell/General Dynamics made their preliminary proposals under shuttle Phase B contracts. References: 44.
1970 Late - Launch Vehicle: Titan. Model: Titan 3M.
  • MOL 1 Nation: USA. Spacecraft: MOL. The first unmanned Gemini-B/Titan 3M qualification flight was planned for late 1970 at the time the program was cancelled. References: 128.
1970 December 2 -
  • Grechko blocking Spiral program. Nation: USSR. Program: Almaz, Salyut. Spacecraft: Spiral OS, Almaz OPS. Kutahkov is now Kamanin's direct superior; Efimov has been sent to a command in Cairo. Two An-22 heavy-lift transports have crashed in Pakistan and the Atlantic (en route to Chile). Kamanin meets with Dementiev and Kazatov at MAP. DOS-7K and Almaz simulator problems and the Spiral spaceplane project are discussed. There is not even a firm program plan for Spiral. Dementiev says this is because of the coolness of Grechko and Kutakhov to the subject. They block any discussion of the matter by the Central Committee. Grechko has written on Spiral - 'this is a fanatasy. We must spend money on more concrete items'. References: 376.
1970 December 2 - 04:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47117-105.
  • Cosmos 381 Nation: USSR. Mass: 710 kg (1,560 lb). Class: Earth. Type: Ionosphere. Spacecraft: Ionosfernaya. Agency: MO SSSR. Perigee: 961 km (597 mi). Apogee: 1,007 km (625 mi). Inclination: 74.00 deg. Period: 104.80 min. COSPAR: 1970-102A. USAF Sat Cat: 4783. References: 2, 6.
1970 December 2 - 07:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.267UG.
  • Astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1970 December 2 - 08:32 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 CRL A04.004-3.
  • HISTAR Test Infrared astronomy mission Nation: USA. Agency: AFCRL. Apogee: 190 km (110 mi). References: 2.
1970 December 2 - 17:00 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/D. LV Configuration: Proton-K/D 252-01.
  • Cosmos 382 Nation: USSR. Program: Lunar L3. Payload: Soyuz 7K-L1E s/n 2K. Mass: 10,380 kg (22,880 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-L1E. Agency: MOM. Perigee: 2,384 km (1,481 mi). Apogee: 5,269 km (3,273 mi). Inclination: 55.90 deg. Period: 171.00 min. COSPAR: 1970-103A. USAF Sat Cat: 4786. Duration: 8,549.30 days. Test of Block D upper stage in its N1 lunar crasher configuration in earth orbit. The three maneuvers simulated the lunar orbit insertion burn; the lunar orbit circularization burn; and the descent burn to bring the LK lunar lander just over the surface. Payload was a modified Soyuz 7K-L1 circumlunar spacecraft, which provided guidance to the Block D and was equipped with television cameras that viewed the behavior of the Block D stage propellants under zero-G conditions.
    Maneuver Summary:
    190km X 300km orbit to 303km X 5038km orbit. Delta V: 982 m/s
    318km X 5040km orbit to 1616km X 5071km orbit. Delta V: 285 m/s
    1616km X 5071km orbit to 2577km X 5082km orbit. Delta V: 1311 m/s
    Total Delta V: 2578 m/s. References: 2, 6, 67, 274.
1970 December 2 - 18:02 GMT - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-3.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1970 December 3 - 13:55 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 383 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 279 km (173 mi). Inclination: 65.40 deg. Period: 89.30 min. COSPAR: 1970-104A. USAF Sat Cat: 4787. Duration: 13.00 days. Decay Date: 1970-12-16. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1970 December 6 - 11:13 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 S69.
  • ESRO S69 X-ray astronomy mission Nation: Europe. Agency: ESRO. Apogee: 187 km (116 mi). References: 2.
1970 December 7 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT56M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 December 7 - 21:34 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 4A. LV Configuration: Black Brant IVA AKF-4A-19.
  • Twilight airglow Aeronomy / x-ray astronomy mission Nation: Canada. Agency: NRCC. Apogee: 770 km (470 mi). References: 2.
1970 December 9 -
  • Funds allocated to Cosmonaut Training Centre only a fraction of what is needed. Nation: USSR. Program: Almaz, Salyut. Spacecraft: Almaz OPS. Kamanin reviews 1970. It has been a good year. The Soviet Union set a duration record with the Soyuz 9 flight, Luna-16 and Lunokhod-1 conducted successful robot missions to the moon, dozens of Kosmos satellites were successfully launched. In the next year cosmonaut training will concentrate on DOS-7K, Almaz, and Soyuz 7KT. The five-year plan for the centre includes construction of 5000 square metres of new laboratories, improved simulators, completion of a water tank for EVA training, and installation of the IF-20 centrifuge. However all of this will cost 11 million roubles, and only 2 to 3 million are likely to be allocated... References: 376.
1970 December 10 - 11:10 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 384 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 203 km (126 mi). Apogee: 292 km (181 mi). Inclination: 72.90 deg. Period: 89.50 min. COSPAR: 1970-105A. USAF Sat Cat: 4791. Duration: 12.00 days. Decay Date: 1970-12-22. Area survey photo reconnaissance satellite; returned film capsule; deployed science capsule. References: 2, 6.
1970 December 10 - 16:27 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk W-NT-36.
  • DLR W-NT-36 Aeronomy mission Nation: Germany. Agency: DLR. Apogee: 270 km (160 mi). References: 2.
1970 December 11 - Launch Site: Baikonur. Launch Complex: LC161/35. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • RVSN Command operational test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1970 December 11 - 11:35 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta N6. LV Configuration: Thor Delta N6 546/D81.
  • NOAA 1 Nation: USA. Program: Tiros. Payload: ITOS A. Mass: 306 kg (674 lb). Class: Earth. Type: Weather. Spacecraft: ITOS. Agency: NOAA. Perigee: 1,423 km (884 mi). Apogee: 1,473 km (915 mi). Inclination: 101.70 deg. Period: 114.80 min. COSPAR: 1970-106A. USAF Sat Cat: 4793. Built for NASA; operated by NOAA. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 2, 6.
  • CEPE Nation: USA. Program: Tiros. Agency: NASA GSF. Perigee: 1,426 km (886 mi). Apogee: 1,484 km (922 mi). Inclination: 101.70 deg. Period: 114.92 min. COSPAR: 1970-106B. USAF Sat Cat: 4794. References: 2, 279.
1970 December 12 - Launch Site: Baikonur. Launch Complex: LC142/34. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • RVSN Command operational test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1970 December 12 - 10:53 GMT - Launch Site: San Marco. Launch Complex: -. Launch Pad: -. Launch Vehicle: Scout. Model: Scout B. LV Configuration: Scout B S175C.
  • Explorer 42 Nation: Italy. Program: Explorer. Payload: SAS A. Mass: 143 kg (315 lb). Class: Solar. Spacecraft: SAS. Agency: NASA GSF. Perigee: 521 km (323 mi). Apogee: 570 km (350 mi). Inclination: 3.00 deg. Period: 95.50 min. COSPAR: 1970-107A. USAF Sat Cat: 4797. Decay Date: 1979-04-05. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1970 December 12 - 13:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M V149-39.
  • Cosmos 385 Nation: USSR. Mass: 680 kg (1,490 lb). Class: Navigation. Spacecraft: Tsiklon. Agency: MO SSSR. Perigee: 973 km (604 mi). Apogee: 980 km (600 mi). Inclination: 74.00 deg. Period: 104.60 min. COSPAR: 1970-108A. USAF Sat Cat: 4799. Military navigation satellite. References: 2, 6.
1970 December 12 - 13:04 GMT - Launch Site: Kourou. Launch Complex: Diamant. Launch Pad: -. Launch Vehicle: Diamant. Model: Diamant B. LV Configuration: Diamant B No. 2.
  • Peole Nation: France. Mass: 70 kg (154 lb). Class: Communications. Spacecraft: Peole. Agency: CNES. Perigee: 634 km (393 mi). Apogee: 750 km (460 mi). Inclination: 15.00 deg. Period: 98.60 min. COSPAR: 1970-109A. USAF Sat Cat: 4801. Decay Date: 1980-06-16. Gathered data from meteorological balloon system. References: 2, 6.
1970 December 14 - 10:02 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB AAD-VB-30.
  • Geminids Ionosphere / meteorites mission Nation: Canada. Agency: NRCC. Apogee: 340 km (210 mi). References: 2.
1970 December 14 - 15:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-2.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1970 December 15 -
  • TsPK Technical Conference Opens Nation: USSR. Kamanin returns from vacation after two weeks at his dacha. Lunokhod was successsfully revived after surviving a lunar night. Venera-7 is set to soft-land on Venus. NII-TsPK holds a science/technology conference on manned spaceflight. 80 papers are presented, with 600 attendees from 39 organisations present. Kamanin talks to Mishin for the first time since the unpleasant phone call in October. References: 376.
1970 December 15 - 1970 December 15 - 03:08 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.470CM.
  • TMA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 208 km (129 mi). References: 2.
1970 December 15 - 05:18 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.471CM.
  • TMA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 214 km (132 mi). References: 2.
1970 December 15 - 07:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.472CM.
  • TMA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 213 km (132 mi). References: 2.
1970 December 15 - 09:04 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.473CM.
  • TMA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 195 km (121 mi). References: 2.
1970 December 15 - 10:00 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 386 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 222 km (137 mi). Apogee: 242 km (150 mi). Inclination: 65.00 deg. Period: 89.10 min. COSPAR: 1970-110A. USAF Sat Cat: 4804. Duration: 13.00 days. Decay Date: 1970-12-28. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1970 December 15 - 11:27 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.474CM.
  • Sodium-Lithium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 215 km (133 mi). References: 2.
1970 December 16 - 04:29 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M V149-31.
  • Cosmos 387 Nation: USSR. Program: Tselina. Mass: 875 kg (1,929 lb). Class: Sigint. Spacecraft: Tselina-O. Agency: MO SSSR. Perigee: 525 km (326 mi). Apogee: 543 km (337 mi). Inclination: 74.00 deg. Period: 95.30 min. COSPAR: 1970-111A. USAF Sat Cat: 4806. Decay Date: 1980-01-19. Possible navigation satellite. Replaced Cosmos 269. References: 2, 6.
1970 December 16 - 09:03 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Apogee: 165 km (102 mi). References: 2.
1970 December 16 - 16:39 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk W-NT-37.
  • DLR W-NT-37 Aeronomy mission Nation: Germany. Agency: DLR. Apogee: 270 km (160 mi). References: 2.
1970 December 17 -
  • Public information policy for DOS/Almaz discussed. Nation: USSR. Program: Almaz, Salyut. Spacecraft: Almaz OPS. Plans for secrecy, public information policy, and arrangements for the upcoming DOS and Almaz space station flights are discussed. References: 376.
1970 December 17 - 19:23 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.418UA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1970 December 18 - 01:00 GMT - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT58M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1970 December 18 - 05:30 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Ionosphere mission Nation: USSR. Apogee: 160 km (90 mi). References: 2.
1970 December 18 - 09:39 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
  • Cosmos 388 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 43. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 271 km (168 mi). Apogee: 505 km (313 mi). Inclination: 71.00 deg. Period: 92.30 min. COSPAR: 1970-112A. USAF Sat Cat: 4811. Completed Operations Date: 1971-05-12. Decay Date: 1971-05-10. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1970 December 18 - 16:15 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
  • Cosmos 389 Nation: USSR. Program: Tselina. Payload: Tselina-D no. 1. Mass: 3,800 kg (8,300 lb). Class: Sigint. Spacecraft: Tselina-D. Agency: MOM. Perigee: 543 km (337 mi). Apogee: 568 km (352 mi). Inclination: 81.20 deg. Period: 95.80 min. COSPAR: 1970-113A. USAF Sat Cat: 4813. Decay Date: 2003-11-24. References: 2, 6.
1970 December 19 -
  • Differences between VVS and Mishin enumerated. Nation: USSR. Program: Salyut, Lunar L3. Flight: Soyuz 10. Lunokhod-1 and Venera-7 missions continue well. The NIITsPK conference is completed, final total 88 papers. The conference has recommended a cautious build-up in manned flight durations - the next mission should be 22 days long, then 26, then 30. But Ustinov has ordered Mishin to ensure that the first flight to DOS will be 30 days long. Kamanin is categorically opposed to this. Kamanin runs through the principal differences between himself and Mishin:
    • Mishin wants to continue work on the N1-L3 moon project. Kamanin thinks the whole thing should be cancelled
    • Kamanin wants the L3 to land on Soviet territory. Mishin wants it to land in the Indian Ocean
    • Mishin wants to make the next manned flight 30 days long. Kamanin wants to limit it to 18 days
    Mishin has the Soviet Ministers (Smirnov), and the Central Committee (Ustinov, Stroganov, etc) behind him. Kamanin has only shaky support from the VVS... References: 376.
1970 December 19 - 03:10 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.11UG.
  • Astronomy mission Nation: USA. Agency: NASA. Apogee: 160 km (90 mi). References: 2.
1970 December 22 - Launch Site: El Arenosillo. Launch Complex: -. Launch Pad: -. Launch Vehicle: INTA. Model: INTA-255. LV Configuration: INTA-255 3.
  • Test mission Nation: Spain. Agency: INTA. Apogee: 132 km (82 mi). References: 2.
1970 December 22 - 08:38 GMT - Launch Site: Vandenberg.