Chronology - Quarter 1 1971 home
topic index

PreviousHomeNext

1971 January 1 - 1971 - Launch Vehicle: Alfa.
  • Alfa SLBM project begun. Nation: Italy. The project for an indigenous Italian ballistic missile was begunby the Italian Navy. Officially it was called a 'technology program intented to develop high power solid-propellant boosters for civil and military applications'. The resulting missile was to be carried on submarines and major surface combatants.
1971 - 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.
1971 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100.
  • Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1971 January -
  • LLTV destroyed in crash at Houston. Nation: USA. Spacecraft: Apollo LLRV. Donald 'Deke' Slayton, then NASA's astronaut chief, said there was no other way to simulate a moon landing except by flying the LLTV. LLRV No. 2, the sole survivor, was eventually returned to Dryden, where it is on display as a silent artifact of the Center's contribution to the Apollo program.
1971 January 3 -
  • Skylab Orbital Workshop dynamic test article delivered. Nation: USA. Program: Skylab. Spacecraft: Skylab. The Orbital Workshop dynamic test article arrived at the Clear Lake Creek Basin adjacent to MSC aboard the barge Orion. It was offloaded on 7 January and moved to the MSC acoustic test facility where it was set up for vibroacoustic testing scheduled to start on 20 January. The acoustic test facility had been checked out previously, and the acoustic environments generated met simulated conditions surrounding the Skylab during Skylab I liftoff and Skylab 1 maximum gravity.
1971 January 5 -
  • VVS Reviews TsKBEM Facilities and Programs Nation: USSR. Program: Salyut, Lunar L3. Spacecraft: Salyut 1, Soyuz 7K-LOK. Two hour meeting between the VVS leadership and Mishin at TsKBEM. Mishin claims he will fly the N1 to orbit this year, and that it will have a payload of 95 to 100 tonnes to low earth orbit. He wants to make 4 to 5 unmanned launches in 1971-1972, followed by one unmanned lunar flyby, culminating in the first Soviet cosmonaut landing on the moon in March 1973. Afterwards the VVS leaders tour the L3 and DOS-7K mock-ups. Mishin asks - Why won't the VVS support his plan for an Indian Ocean landing for the L3? Why is the VVS against a 30-day duration for the first DOS flight? Why isn't the VVS training engineer-cosmonauts as pilots? Kutakhov replies that these are decisions that have to be made by aviation specialists, not by engineers or chief designers. The General Staff supports the VVS position. References: 376.
1971 January 7 - 20:01 GMT - Launch Site: Point Barrow. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.365GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 122 km (75 mi). References: 2.
1971 January 7 - 20:30 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.372GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 131 km (81 mi). References: 2.
1971 January 8 - 21:41 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.016-3.
  • Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 278 km (172 mi). References: 2.
1971 January 8 - 22:11 GMT - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena V144D.
  • Re-entry Vehicle test Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1971 January 8 - 22:31 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.015-2.
  • Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 276 km (171 mi). References: 2.
1971 January 9 -
  • VVS Reviews TsKBM Facilities and Programs Nation: USSR. Program: Almaz, Salyut. Spacecraft: Salyut 1, Almaz OPS. The VVS leadership visits Chelomei's facility at Reutov. Kamanin recalls first seeting the Almaz mock-up five years earlier - it was already fully defined then. But it was only in August 1970 that a resolution was issued setting a firm schedule: Chelomei was to start flight trails in the second half of 1971, and the station was to enter service in 1972. Mishin is proposing to cancel Almaz and build 10 DOS stations instead. Mishin currently supervises five design bureaux, 60,000 workers, and is working on Soyuz, 7K-S, L3, DOS-7K, and a very few other projects. Chelomei has only one design bureau and 8,000 workers. Yet he has produced well-designed, mass-produced cruise missiles for the Navy, over 1,000 ICBM's for the RVSN, and the high-quality UR-500 Proton launch vehicle. Almaz could have flown on time if Ustinov had allowed Chelomei just 10% of the resources he has let Mishin squander on DOS. Chelomei easily agrees with the VVS to a mutual schedule for Almaz crew training, crew composition, etc. The contrast with the argumentative Mishin couldn't be greater. References: 376.
1971 January 9 -
  • Shatalov comes to leadership attention after good work on Pompidou visit. Nation: USSR. The leadership wants to appoint Shatalov as a space adviser to the General Staff. Kamanin wants him as Deputy Commander of TsPK. References: 376.
1971 January 11 - Launch Site: Kwajalein. Launch Complex: Meck. Launch Pad: -. Launch Vehicle: Spartan. LV Configuration: Spartan ABM 800021.
  • SAFEGUARD M1-30 Interceptor mission Nation: USA. Agency: USA. Apogee: 100 km (60 mi). References: 2.
1971 January 11 - Launch Site: Kwajalein. Launch Complex: Meck. Launch Pad: -. Launch Vehicle: Spartan. LV Configuration: Spartan ABM 800024.
  • SAFEGUARD M1-30 Interceptor mission Nation: USA. Agency: USA. Apogee: 100 km (60 mi). References: 2.
1971 January 11 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • SSTTP M1-30 Target mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1971 January 12 - 07:50 GMT - Launch Site: Point Barrow. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.366GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 116 km (72 mi). References: 2.
1971 January 12 - 09:30 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 390 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 196 km (121 mi). Apogee: 276 km (171 mi). Inclination: 65.00 deg. Period: 89.20 min. COSPAR: 1971-001A. USAF Sat Cat: 4845. Duration: 13.00 days. Decay Date: 1971-01-25. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1971 January 12 - 20:53 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.373GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 133 km (82 mi). References: 2.
1971 January 13 - 20:10 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II ADD-2-124.
  • O2 profile Aeronomy mission Nation: Canada. Agency: NRCC. Apogee: 146 km (90 mi). References: 2.
1971 January 14 -
  • VVS should support Almaz and Spiral. Nation: USSR. Program: Almaz, Salyut. Spacecraft: Salyut 1, Spiral OS. Kamanin discusses with Kutakhov the need for the VVS to back Chelomei rather than Mishin. As for the Spiral, the support of Dementiev, Afanasyev, Kalmykov, and Zverev have been lined up for the program. But Grechko is still blocking it. And Kutakhov is unwilling to challenge Grechko on the issue. References: 376.
1971 January 14 - 12:00 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
  • Cosmos 391 Nation: USSR. Program: DS. Payload: DS-P1-I s/n 11. Mass: 300 kg (660 lb). Class: Military. Type: Target. Spacecraft: DS-P1-I. Agency: MO SSSR. Perigee: 267 km (165 mi). Apogee: 803 km (498 mi). Inclination: 70.90 deg. Period: 95.30 min. COSPAR: 1971-002A. USAF Sat Cat: 4847. Completed Operations Date: 1971-04-01. Decay Date: 1972-02-21. Operational radar target for the ABM forces. References: 2, 6, 99.
1971 January 15 -
  • Spiral to be raised at VVS Soviet. Nation: USSR. Spacecraft: Spiral OS. Kamanin manges to get to Zakahrov, who agrees to take the Spiral issue to the Military Soviet of the VVS. Leonov and Nikolayev review Kamanin's new draft decree to be presented to he Military Soviet. The DOS-7K is two weeks behind schedule for the planned 15 March launch date. References: 376.
1971 January 15 - 20:30 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk MUMP 10.
  • Aeronomy mission Nation: USA. Agency: USAF. Apogee: 289 km (179 mi). References: 2.
1971 January 16 -
  • Lunokhod 1 has completed its lunar activities. Nation: USSR. Spacecraft: Lunokhod. Kamanin's son, also a VVS pilot, is being sent to Hanoi for service. Kamanin writes a letter to Keldysh on the naming of lunar craters for deceased cosmonauts. References: 376.
1971 January 16 - 00:55 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk MUMP-9.
  • MUMP 9 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 297 km (184 mi). References: 2.
1971 January 16 - 02:00 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-210. LV Configuration: S-210-4.
  • Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 115 km (71 mi). References: 2.
1971 January 16 - 07:15 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-30.
  • Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 357 km (221 mi). References: 2.
1971 January 16 - 23:32 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois SECEDE R12.
  • NUTMEG Aeronomy mission Nation: USA. Agency: USAF. Apogee: 144 km (89 mi). References: 2.
1971 January 17 - 14:48 GMT - Launch Site: Kiruna. Launch Complex: C. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C37/2.
  • ESRO C37 / 2 MPE Ba Ionosphere / barium release mission Nation: Europe. Agency: ESRO. Apogee: 215 km (133 mi). References: 2.
1971 January 17 - 15:33 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk DLR A-NT-39.
  • MPE Barium release / Brigitte Ionosphere / fields mission Nation: Germany. Agency: DLR. Apogee: 328 km (203 mi). References: 2.
1971 January 18 -
  • Spiral controversy continues. Nation: USSR. Spacecraft: Spiral OS. Kutakhov flies to Minsk, with the draft decree to be submitted to the Military Soviet still not approved. The leadership have many questions, especially concerning the Spiral project. References: 376.
1971 January 19 - 19:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee D. LV Configuration: Astrobee D Robin.
  • AFCRL 71-1 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 146 km (90 mi). References: 2.
1971 January 20 -
  • Mishin pushing 'Big Orbital Station'. Nation: USSR. Program: Almaz, Salyut. Spacecraft: Almaz OPS, MKBS. Mishin is attempting to set up a separate training centre for civilian cosmonauts at the Moscow Aviation Institute. Mishin and the civilian cosmonauts come to view the TsPK premises to get ideas. This is a new attack by Mishin, in Kamanin's eyes. Mishin has been ill for a long time, but it doesn't stop him from meddling in the details of work of his deputies. Now they are working on a Big Orbital Station (BOS) for 9-12 crew. This amounts to nothing more than a new move against Chelomei. Mishin is intent on monopolising manned spaceflight at any cost. He attempts to take over any other such projects allocated to Chelomei or Kozlov. References: 376.
1971 January 20 - 11:24 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
  • Meteor 1-07 Nation: USSR. Payload: Meteor M no. 7. Mass: 3,800 kg (8,300 lb). Class: Earth. Type: Weather. Spacecraft: Meteor M. Agency: MOM. Perigee: 538 km (334 mi). Apogee: 550 km (340 mi). Inclination: 81.20 deg. Period: 95.50 min. COSPAR: 1971-003A. USAF Sat Cat: 4849. Decay Date: 2005-06-14. Acquisition of meteorological information needed for use by the weather service. References: 2, 6.
1971 January 20 - 23:45 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois SECEDE R13.
  • PLUM Aeronomy mission Nation: USA. Agency: USAF. Apogee: 182 km (113 mi). References: 2.
1971 January 21 -
  • X-24 Flight 21 Nation: USA. Payload: X-24A flight 21. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Manke. Maximum Speed - 1093 kph. Maximum Altitude - 15819 m. Flight Time - 462 sec. References: 49, 97.
1971 January 21 - 02:32 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB AKD-VB-27.
  • Auroral Aurora / ionosphere / plasma mission Nation: Canada. Agency: NRCC. Apogee: 258 km (160 mi). References: 2.
1971 January 21 - 08:40 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 392 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 278 km (172 mi). Inclination: 65.00 deg. Period: 89.30 min. COSPAR: 1971-004A. USAF Sat Cat: 4872. Duration: 12.00 days. Decay Date: 1971-02-02. Area survey photo reconnaissance satellite; returned film capsule. References: 2, 6.
1971 January 21 - 18:18 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee D. LV Configuration: Astrobee D Robin.
  • AFCRL 71-2 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 130 km (80 mi). References: 2.
1971 January 21 - 18:28 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 23B. LV Configuration: Titan 23B 23B-8 (3B-30).
  • OPS 7776 Nation: USA. Payload: KH-8 no. 30 / Agena D. Mass: 3,000 kg (6,600 lb). Class: Surveillance. Type: Military. Spacecraft: KH-8. Agency: NRO/USAF. Perigee: 139 km (86 mi). Apogee: 418 km (259 mi). Inclination: 110.90 deg. Period: 90.10 min. COSPAR: 1971-005A. USAF Sat Cat: 4874. Decay Date: 1971-02-09. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1971 January 21 - 19:02 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee D. LV Configuration: Astrobee D Robin.
  • AFCRL 71-3 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 129 km (80 mi). References: 2.
1971 January 21 - 19:38 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee D. LV Configuration: Astrobee D Robin.
  • AFCRL 71-4 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 132 km (82 mi). References: 2.
1971 January 21 - 20:19 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee D. LV Configuration: Astrobee D Robin.
  • AFCRL 71-5 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 132 km (82 mi). References: 2.
1971 January 21 - 21:02 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee D. LV Configuration: Astrobee D Robin.
  • AFCRL 71-6 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 127 km (78 mi). References: 2.
1971 January 22 -
  • Low and Anders visit the Gagarin Training Centre. Nation: USSR. They are very interested in the Soyuz and Volga trainers. References: 376.
1971 January 22 - 20:22 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.116IE.
  • Ferdinand 26 / Polar 2 Plasma mission Nation: USA. Agency: NASA. Apogee: 253 km (157 mi). References: 2.
1971 January 23 -
  • Meeting of VVS leadership. Nation: USSR. Spacecraft: Spiral OS. Kamanin reviews his public relations operations. In ten years the cosmonauts have made 6,000 speeches and gone on 200 publicity tours. Tereshkova is the most in demand. 30 documentary films have been produced, as well as hundreds of books and brochures. The Star City Museum had 13,000 visitors in 1970. References: 376.
1971 January 23 - 02:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.260GG.
  • Astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1971 January 23 - 04:44 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB ADD-VB-24.
  • Auroral VUV Aurora / ionosphere / plasma mission Nation: Canada. Agency: NRCC. Apogee: 375 km (233 mi). References: 2.
1971 January 23 - 13:20 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-35.
  • Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 338 km (210 mi). References: 2.
1971 January 23 - 20:08 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Ionosphere mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 January 24 - 02:00 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-34.
  • Sco X-1 X-ray astronomy / solar ultraviolet mission Nation: Japan. Agency: ISAS. Apogee: 328 km (203 mi). References: 2.
1971 January 25 -
  • Cosmonauts on public relations duty. Nation: USSR. A record number of cosmonauts are away from the training centre on public relations trips. References: 376.
1971 January 25 - 08:19 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.324GE.
  • PCA particle spectra Plasma mission Nation: USA. Agency: NASA. Apogee: 160 km (90 mi). References: 2.
1971 January 25 - 11:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.318UA.
  • JHU UVT F6 (Venus) Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 160 km (90 mi). References: 2.
1971 January 25 - 12:38 GMT - Launch Site: Kiruna. Launch Complex: C. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C60/1.
  • ESRO C60 / 1 Chemical release / particles mission Nation: Europe. Agency: ESRO. Apogee: 175 km (108 mi). References: 2.
1971 January 25 - 14:26 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.46UA.
  • JHU Airglow 10 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 245 km (152 mi). References: 2.
1971 January 25 - 15:12 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.432GE.
  • PCA particle spectra Plasma mission Nation: USA. Agency: NASA. Apogee: 160 km (90 mi). References: 2.
1971 January 26 -
  • ECS technology review. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1, MKBS, Aelita. Keldysh heads a review of spacecraft environmental control system development. The work of the IMBP is not well organised. They have been developing systems for eight years with no concrete results. G I Voronin is responsible for oxygen regenerator and thermal regulation systems; G I Severin, for space suits; O G Gazenko for biosensors, medicines, and space food. Two problems need to be solved: to understand and counter the effects of zero gravity on the human organism; and to develop a reliable environmental control system with a guaranteed life of two to three years. Keldysh declares that in the next five to ten years the Soviet Union will not fly space stations with artificial gravity. Therefore, due to the inevitable deterioration of the human body in zero gravity, crews will have to be rotated every 30 to 60 days. Development must continue with an eye to supporting eventual lunar bases and manned expeditions to Mars. References: 376.
1971 January 26 - 00:36 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36A. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3C Centaur. LV Configuration: SLV-3C Centaur AC-25 / Centaur D-1A 5005C.
  • Intelsat 4 F-2 Nation: International. Program: Intelsat. Mass: 706 kg (1,556 lb). Class: Communications. Spacecraft: Intelsat 4. Agency: Intelsat. Perigee: 36,151 km (22,463 mi). Apogee: 36,236 km (22,515 mi). Inclination: 15.30 deg. Period: 1,457.00 min. COSPAR: 1971-006A. USAF Sat Cat: 4881. Completed Operations Date: 1983-05-11. Launch vehicle put payload into geosynchronous transfer orbit; the satellite performed the apogee burn and positioned itself in geosynchronous orbit over the Atlantic Ocean at 24.5 deg W. Subsequently at 23 deg W in 1971-1975; over the Atlantic Ocean 1-6 deg W in 1976-1980; over the Atlantic Ocean 0-5 deg E in 1980-1983. As of 3 September 2001 at 31.91 deg E drifting at 5.168 deg W per day. As of 2006 Dec 18 located at 133.93E drifting at 5.166W degrees per day. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 2, 6, 278.
1971 January 26 - 10:50 GMT - Launch Site: Kiruna. Launch Complex: C. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C60/2.
  • ESRO C60 / 2 Chemical release / particles mission Nation: Europe. Agency: ESRO. Apogee: 167 km (103 mi). References: 2.
1971 January 26 - 12:44 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
  • Cosmos 393 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 34. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 272 km (169 mi). Apogee: 485 km (301 mi). Inclination: 71.00 deg. Period: 92.10 min. COSPAR: 1971-007A. USAF Sat Cat: 4884. Completed Operations Date: 1971-06-12. Decay Date: 1971-06-16. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1971 January 26 - 13:22 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel ESRO P40/1.
  • ESRO P40 / 1 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 145 km (90 mi). References: 2.
1971 January 26 - 17:23 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB AMD-VB-26.
  • Airglow Ionosphere / solar mission Nation: Canada. Agency: NRCC. Apogee: 282 km (175 mi). References: 2.
1971 January 26 - 22:58 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. LV Configuration: Terrier Tomahawk SECEDE.
  • Cert.Round (Probe C) test Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi). References: 2.
1971 January 26 - 23:50 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois SECEDE R14.
  • REDWOOD Aeronomy mission Nation: USA. Agency: USAF. Apogee: 252 km (156 mi). References: 2.
1971 January 27 -
  • DOS training conflicts. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1, Soyuz 7KT-OK. Beregovoi, Leonov, and Shatalov go to TsKBEM to review the training plan for the DOS-7K station at the KIS (Experimental Control Station) facility. Mishin wants the crew of Soyuz s/n 32 to be working aboard the 'live' spacecraft on 3-4 February, but they need to be at the cosmodrome on those dates for training on the Svinets ICBM detector experiment. This conflicts with Mishin's schedule for availability of a 'live' Soyuz for training. Mishin still wants, completely unrealistically, to launch on the day of the 24th Party Conference. References: 376.
1971 January 27 -
  • Kamanin lists Soviet space management failures. Nation: USSR. Spacecraft: Soyuz 7K-LOK, LK. It is obvious to Kamanin from the ECS conference that there are many mistakes in the organization of the Soviet space program. There is no single agency directing the program, like the American NASA. There is not only no five year plan for manned spaceflight, there is not even a plan for next year! Decisions on manned space are made erratically by unqualified members of the leadership. There is no single manager of military space projects. Ustinov, Smirnov, Keldysh, and Karas at GUKOS are all pulling in different directions. Ustinov, Smirnov, and Keldysh don't give space more than 10% of their working time. References: 376.
1971 January 27 - Launch Site: Vandenberg. Launch Complex: LF08. Launch Pad: -. Launch Vehicle: Minuteman 3.
  • OLD FOX 04M demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1971 January 27 - 23:02 GMT - Launch Site: Kiruna. Launch Complex: C. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C78/1.
  • ESRO C78 / 1 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 140 km (80 mi). References: 2.
1971 January 28 -
  • Spiral negotiations continue. Nation: USSR. Spacecraft: Spiral OS. An article Kamanin has written on aircraft designer Ilyushin has been published in Pravda. Kamanin is impressed by a new book by Orlov on possible civilian medical applications of technology developed for spaceflight. Negotiations continue with the Military Soviet on the resolution on future manned military space projects. References: 376.
1971 January 28 - 05:10 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.409II.
  • ISRO 10.37 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 163 km (101 mi). References: 2.
1971 January 28 - 05:40 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.410II.
  • ISRO 10.38 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 189 km (117 mi). References: 2.
1971 January 28 - 15:55 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk DLR A-NT-38.
  • MPE Barium release / Erika Ionosphere / fields mission Nation: Germany. Agency: DLR. Apogee: 276 km (171 mi). References: 2.
1971 January 28 - 18:33 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S46/2.
  • ESRO S46 / 2 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 218 km (135 mi). References: 2.
1971 January 28 - 22:57 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. LV Configuration: Terrier Tomahawk SECEDE R15.
  • REDWOOD (Probe F) Aeronomy / Fields mission Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi). References: 2.
1971 January 29 -
  • Space vehicle for the Apollo 14 mission determined ready for launch Nation: USA. Program: Apollo. Flight: Apollo 14. The space vehicle for the Apollo 14 mission was determined ready for launch on January 31. The Flight Readiness Review had been held at KSC on December 17, 1970; all required action and open work had been completed; and the Pre-Liftoff Readiness Review had been favorably completed January 29. References: 16.
1971 January 29 -
  • Plans for test of DOS ABM sensor technology at Baikonur. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Three DOS-7K crews are to fly on two Tu-104's to Baikonur on 30 January. The Tu-104's are fitted with the Svinets equipment, which the cosmonauts will use to capture spectral data on two rocket launches. This training will prepare them for use of the Svinets equipment aboard the DOS station. Lots of bigwigs from the VVS plan to tag along as well. References: 376.
1971 January 29 - 02:10 GMT - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • FOT GT90B Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1971 January 29 - 08:25 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL1001.
  • XRB anisotropy X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 203 km (126 mi). References: 2.
1971 January 29 - 17:03 GMT - Launch Site: Keweenaw. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.167GI.
  • Ionosphere mission Nation: USA. Agency: NASA. Apogee: 132 km (82 mi). References: 2.
1971 January 29 - 19:48 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Boosted Arcas 2. LV Configuration: Boosted Arcas 2 NASA 15.50UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 122 km (75 mi). References: 2.
1971 January 29 - 23:52 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois SECEDE R16.
  • OLIVE (352 kg) Aeronomy mission Nation: USA. Agency: USAF. Apogee: 190 km (110 mi). References: 2.
1971 January 30 -
  • Warsaw Pact officers tour Gagarin Cosmonaut Training Centre. Nation: USSR. The TsPK is visited by participants in a meeting of the Warsaw Pact General Staff. This amounts to 29 generals, 2 to 3 from each country of the pact. References: 376.
1971 January 31 - 13:55 GMT - Launch Site: Keweenaw. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.373GI.
  • Ionosphere mission Nation: USA. Agency: NASA. Apogee: 185 km (114 mi). References: 2.
1971 January 31 - 21:03 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Saturn V. Model: Saturn V. LV Configuration: Saturn V SA-509.
  • Apollo 14 Nation: USA. Program: Apollo. Payload: Apollo CSM 110 / Apollo LM 8 / ALSEP / S-IVB-509. Mass: 29,230 kg (64,440 lb). Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo CSM. Location of Spacecraft: United States Astronaut Hall of Fame, Titusville, FL. Agency: NASA MSC. Perigee: 170 km (100 mi). Apogee: 183 km (113 mi). Inclination: 31.12 deg. Period: 88.18 min. COSPAR: 1971-008A. USAF Sat Cat: 4900. Duration: 9.00 days. Decay Date: 1971-02-09. Crew: Mitchell, Roosa, Shepard. Flight: Apollo 14. The Apollo 14 (AS-509) mission - manned by astronauts Alan B. Shepard, Jr., Stuart A. Roosa, and Edgar D. Mitchell - was launched from Pad A, Launch Complex 39, KSC, at 4:03 p.m. EST January 31 on a Saturn V launch vehicle. A 40-minute hold had been ordered 8 minutes before scheduled launch time because of unsatisfactory weather conditions, the first such delay in the Apollo program. Activities during earth orbit and translunar injection were similar to those of the previous lunar landing missions. However, during transposition and docking, CSM 110 Kitty Hawk had difficulty docking with LM-8 Antares. A hard dock was achieved on the sixth attempt at 9:00 p.m. EST, 1 hour 54 minutes later than planned. Other aspects of the translunar journey were normal and proceeded according to flight plan. A crew inspection of the probe and docking mechanism was televised during the coast toward the moon. The crew and ground personnel were unable to determine why the CSM and LM had failed to dock properly, but there was no indication that the systems would not work when used later in the flight.

    Apollo 14 entered lunar orbit at 1:55 a.m. EST on February 4. At 2:41 a.m. the separated S-IVB stage and instrument unit struck the lunar surface 174 kilometers southeast of the planned impact point. The Apollo 12 seismometer, left on the moon in November 1969, registered the impact and continued to record vibrations for two hours.

    After rechecking the systems in the LM, astronauts Shepard and Mitchell separated the LM from the CSM and descended to the lunar surface. The Antares landed on Fra Mauro at 4:17 a.m. EST February 5, 9 to 18 meters short of the planned landing point. The first EVA began at 9:53 a.m., after intermittent communications problems in the portable life support system had caused a 49-minute delay. The two astronauts collected a 19.5-kilogram contingency sample; deployed the TV, S-band antenna, American flag, and Solar Wind Composition experiment; photographed the LM, lunar surface, and experiments; deployed the Apollo lunar surface experiments package 152 meters west of the LM and the laser-ranging retroreflector 30 meters west of the ALSEP; and conducted an active seismic experiment, firing 13 thumper shots into the lunar surface.

    A second EVA period began at 3:11 a.m. EST February 6. The two astronauts loaded the mobile equipment transporter (MET) - used for the first time - with photographic equipment, tools, and a lunar portable magnetometer. They made a geology traverse toward the rim of Cone Crater, collecting samples on the way. On their return, they adjusted the alignment of the ALSEP central station antenna in an effort to strengthen the signal received by the Manned Space Flight Network ground stations back on earth.

    Just before reentering the LM, astronaut Shepard dropped a golf ball onto the lunar surface and on the third swing drove the ball 366 meters. The second EVA had lasted 4 hours 35 minutes, making a total EVA time for the mission of 9 hours 24 minutes. The Antares lifted off the moon with 43 kilograms of lunar samples at 1:48 p.m. EST February 6.

    Meanwhile astronaut Roosa, orbiting the moon in the CSM, took astronomy and lunar photos, including photos of the proposed Descartes landing site for Apollo 16.

    Ascent of the LM from the lunar surface, rendezvous, and docking with the CSM in orbit were performed as planned, with docking at 3:36 p.m. EST February 6. TV coverage of the rendezvous and docking maneuver was excellent. The two astronauts transferred from the LM to the CSM with samples, equipment, and film. The LM ascent stage was then jettisoned and intentionally crashed on the moon's surface at 7:46 p.m. The impact was recorded by the Apollo 12 and Apollo 14 ALSEPs.

    The spacecraft was placed on its trajectory toward earth during the 34th lunar revolution. During transearth coast, four inflight technical demonstrations of equipment and processes in zero gravity were performed.

    The CM and SM separated, the parachutes deployed, and other reentry events went as planned, and the Kitty Hawk splashed down in mid-Pacific at 4:05 p.m. EST February 9 about 7 kilometers from the recovery ship U.S.S. New Orleans. The Apollo 14 crew returned to Houston on February 12, where they remained in quarantine until February 26.

    All primary mission objectives had been met. The mission had lasted 216 hours 40 minutes and was marked by the following achievements:

    • Third manned lunar landing mission and return.
    • Use of mobile equipment transporter (MET).
    • Payload of 32,500 kilograms placed in lunar orbit.
    • Distance of 3.3 kilometers traversed on lunar surface.
    • Payload of 43.5 kilograms returned from the lunar surface.
    • Lunar surface stay time of 33 hours.
    • Lunar surface EVA of 9 hours 47 minutes.
    • Use of shortened rendezvous technique.
    • Service propulsion system orbit insertion.
    • Active seismic experiment.
    • Inflight technical demonstrations.
    • Extensive orbital science period during CSM solo operations.
    References: 2, 6, 16, 26, 27, 33,60.
  • Apollo 14 LM Nation: USA. Program: Apollo. Payload: Apollo LM 8. Mass: 15,279 kg (33,684 lb). Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo LM. Agency: NASA MSC. Perigee: 170 km (100 mi). Apogee: 183 km (113 mi). Inclination: 31.12 deg. Period: 88.18 min. COSPAR: 1971-008x. USAF Sat Cat: 4900. Duration: 9.00 days. Decay Date: 1971-02-09. Flight: Apollo 14. References: 2, 6, 16, 26, 27, 33,60.
1971 February 1 -
  • Taifun-1 accepted into military service. Nation: USSR. Spacecraft: Taifun-1. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On adoption of the Taifun-1 into armaments' was issued. References: 474.
1971 February 1 -
  • Salyut shipped to Baikonur Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. The first DOS station was shipped in to Baikonur in an incomplete state. Work continued to complete it day and night without break. The old MIK at Baikonur was used to prepare the Soyuz launch vehicle and 7K-TOK ferry spacecraft. The station was to be called Zarya, or 'Dawn', but the name was changed just before launch to prevent confusion with the secret Chinese manned spacecraft of the same name. Additional Details: Salyut shipped to Baikonur. References: 367.
1971 February 1 -
  • Military Soviet of the VVS considers manned space plans - Day 1. Nation: USSR. Spacecraft: Spiral OS. The Military Soviet of the VVS meets from 10:00 to 15:00. Kamanin's draft decree is debated. The Apollo 14 launch has bolstered interest in Soviet spaceflight. Problems with the decree are identified, but solved. Kamanin is particularly happy that mention is made of good use of crewed spacecraft designs as opposed to total automation. References: 376.
1971 February 1 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Pad: -. Launch Vehicle: S. Model: JCR. LV Configuration: JCR-5.
  • Test mission Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi). References: 2.
1971 February 1 - 22:55 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. LV Configuration: Terrier Tomahawk SECEDE R17. FAILURE: Failure.
  • SPRUCE II (Probe B) Aeronomy / Fields mission Nation: USA. Agency: Sandia. Apogee: 0 km ( mi). References: 2.
1971 February 1 - 22:57 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. LV Configuration: Terrier Tomahawk SECEDE R18.
  • SPRUCE II (Probe C) Ionosphere / fields mission Nation: USA. Agency: Sandia. Apogee: 260 km (160 mi). References: 2.
1971 February 2 -
  • Military Soviet of the VVS considers manned space plans - Day 2. Nation: USSR. Spacecraft: Spiral OS. Kamanin waits and waits to give his speech on the second day of the VVS Military Soviet. It is constantly postponed. He spends 16 hours waiting 'on-call'. This demonstrates to him the poor organisation of the military leadership. References: 376.
1971 February 2 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. Model: UR-100M.
  • First State trials launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1971 February 2 - 15:35 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. LV Configuration: Terrier Tomahawk SECEDE R19.
  • QUINCE II (Probe A) Aeronomy / ionosphere / Fields mission Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi). References: 2.
1971 February 2 - 15:36 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. LV Configuration: Terrier Tomahawk SECEDE R20.
  • QUINCE II (Probe E) Aeronomy / Fields mission Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi). References: 2.
1971 February 3 -
  • First Svinets test successful. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Leonov reports that the Tu-104 was ready last night for the flight to observe a rocket launch using the Svinets device. All went normally. The second launch will be made tonight at 20:00. References: 376.
1971 February 3 - Launch Site: Vandenberg. Launch Complex: LF24. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • FOT GT101F Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1971 February 3 - 01:41 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta M. LV Configuration: Thor Delta M 560/D82.
  • NATO 2 Nation: NATO. Program: NATO. Payload: NATO IIB. Mass: 243 kg (535 lb). Class: Communications. Type: Military. Spacecraft: NATO 1. Agency: NATO. Perigee: 35,772 km (22,227 mi). Apogee: 35,802 km (22,246 mi). Inclination: 13.90 deg. Period: 1,436.10 min. COSPAR: 1971-009A. USAF Sat Cat: 4902. Completed Operations Date: 1984-06-01. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Atlantic Ocean at 26 deg W in 1971-1975?; over the Americas at 105 deg W in 1976-1983; over the Americas at 110 deg W in 1983; over the Americas at 105 deg W in 1983-1998 As of 5 September 2001 located at 104.88 deg W drifting at 0.004 deg W per day. As of 2007 Mar 9 located at 105.24W drifting at 0.007W degrees per day. References: 2, 6.
1971 February 4 -
  • X-24 Flight 22 Nation: USA. Payload: X-24A flight 22. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Powell. Powell's check flight, glide. Maximum Speed - 700 kph. Maximum Altitude - 13716 m. Flight Time - 235 sec. References: 49, 97.
1971 February 4 -
  • Second Svinets test successful. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. The DOS crews return from Tyuratam. The second missile launch was observed successfully by the Svinets apparatus as well. Cosmonaut teams are assigned to public relations tours of Egypt, USA, Italy, Viet Nam, and Hungary. References: 376.
1971 February 4 - 22:45 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3E-19.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1971 February 5 -
  • Soviet view of Apollo 14. Nation: USSR. Program: Apollo, Lunar L3. Apollo 14 successfully lands on the moon. Kamanin notes that the Soviet Union is now five to six years behind, due to the mistakes of Mishin, Keldysh, Smirnov, and Ustinov. Shonin is training on Soyuz s/n 32 at the KIS of TsKBEM. References: 376.
1971 February 5 - 05:20 GMT - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT60M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1971 February 5 - 09:18 GMT -
  • Apollo 14 lands on the moon Nation: USA. Flight: Apollo 14. After rechecking the systems in the LM, astronauts Shepard and Mitchell separated the LM from the CSM and descended to the lunar surface. Shepard piloted the spacecraft to a routine landing at 09:18:11 GMT about 350 miles (563 kilometers) west-southwest of the center of the moon's visible side. Antares was only 175 feet (53 meters) from its targeted landing site. Additional Details: Apollo 14 lands on the moon.
1971 February 5 - 14:42 GMT -
  • EVA Apollo 14-1 Nation: USA. Program: Apollo. Class: Manned. Type: Lunar lander. Spacecraft: Apollo LM. Crew: Shepard, Mitchell. Flight: Apollo 14. EVA Duration: 0.20 days. Explored lunar surface near LM and deployed ALSEP unmanned scientific station equipment. References: 66.
1971 February 5 - 22:46 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 4B. LV Configuration: Black Brant IVB AKF-4B-24.
  • Impedance dipole Aurora / ionosphere / meteorology mission Nation: Canada. Agency: NRCC. Apogee: 784 km (487 mi). References: 2.
1971 February 6 - 1971 February 6 -
  • Incident with Shonin during DOS training. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. The training session at KIS yesterday was subverted by Shonin's drunkenness. Kamanin investigates the matter all day. Shonin is said to have brought vodka to the KIS and consumed vodka during the session. Kamanin confronted him, but of course he is sober now. Kamanin cannot understand the man, He has known him for eleven years and thought him a competent person. References: 376.
1971 February 6 - 08:11 GMT -
  • EVA Apollo 14-2 Nation: USA. Program: Apollo. Class: Manned. Type: Lunar lander. Spacecraft: Apollo MET. Crew: Shepard, Mitchell. Flight: Apollo 14. EVA Duration: 0.19 days. Attempted to reach rim of Cone Crater on moonwalk with ''golf cart'' for hauling equipment. References: 66.
1971 February 6 - 18:30 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 S80/1.
  • ESRO S80 / 1 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 222 km (137 mi). References: 2.
1971 February 6 - 23:22 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 S80/2.
  • ESRO S80 / 2 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 226 km (140 mi). References: 2.
1971 February 7 - 03:45 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 S80/3.
  • ESRO S80 / 3 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 214 km (132 mi). References: 2.
1971 February 8 -
  • Repercussions of Shonin incident. Nation: USSR. Program: Salyut. Kamanin has a meeting with Leonov and Shonin on the KIS incident. Shonin claims he was sober. Mishin calls. He says Khrunov and Shonin were not ready for training anyway; they had to be led by the nose the whole time. He would prefer that Yeliseyev, Kubasov, and Rukavishnikov be assigned to the mission. References: 376.
1971 February 8 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • FOT GT91B Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1971 February 8 - 13:56 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.51UA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 265 km (164 mi). References: 2.
1971 February 9 -
  • M2 Flight 21 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 5. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Gentry. Maximum Speed - 755 kph. Maximum Altitude - 13716 m. Flight Time - 241 sec. References: 49, 97.
1971 February 9 -
  • Skylab Orbital Workshop management review. Nation: USA. Program: Skylab. Spacecraft: Skylab. An Orbital Workshop management review was conducted at McDonnell Douglas. Representatives from McDonnell Douglas, NASA Hq, KSC, MSFC, and MSC attended. Significant agenda items included the program schedule, engineering changes, design status, component tests, and procurement status. The OWS flight module was about three months behind schedule. The component development and qualification testing was also behind schedule. McDonnell Douglas reorganized the procurement activity and was making a significant effort to improve this area since it directly impacted the schedule slip.
1971 February 9 - 18:48 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65027-119.
  • Cosmos 394 Nation: USSR. Payload: DS-P1-M s/n 2. Mass: 650 kg (1,430 lb). Class: Military. Type: ASAT Target. Spacecraft: DS-P1-M. Agency: MO SSSR. Perigee: 522 km (324 mi). Apogee: 552 km (342 mi). Inclination: 65.80 deg. Period: 95.40 min. COSPAR: 1971-010A. USAF Sat Cat: 4922. Completed Operations Date: 1972-02-29. Target for IS ASAT systems tests. First test using Yangel-designed lighter, cheaper target launched by Kosmos 11K65M booster from Plesetsk. References: 2, 6, 99, 272.
1971 February 9 -
  • Landing of Apollo 14 Nation: USA. Program: Apollo. Flight: Apollo 14. The CM and SM separated, the parachutes deployed, and other reentry events went as planned, and the Kitty Hawk splashed down in mid-Pacific at 21:05 GMT 7 kilometers from the recovery ship U.S.S. New Orleans. The Apollo 14 crew returned to Houston on February 12, where they remained in quarantine until February 26. All primary mission objectives had been met. Additional Details: Landing of Apollo 14.
1971 February 12 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. Model: UR-100M.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1971 February 13 - Launch Vehicle: Shuttle.
  • Shuttle SSME Award Nation: USA. North American Rockwell's Rocketdyne division was awarded NASA contract NAS8-40000 for development of the space shuttle main engine, beating out Pratt and Whitney and Aerojet. This was the only large liquid propellant rocket motor scheduled to be developed in the United States for decades and a crushing blow to the losers. Both felt that their designs were superior to that of Rocketdyne, but Rocketdyne had become NASA's 'house' for main rocket engines. References: 44.
1971 February 14 - 08:17 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.110UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 February 15 -
  • Medical verdict on Shonin. Nation: USSR. Program: Salyut. Shonin is examined by VVS physicians. They believe he became a secret drinker after his October 1969 spaceflight. References: 376.
1971 February 16 - 04:00 GMT - Launch Site: Kagoshima. Launch Complex: M. Launch Pad: -. Launch Vehicle: Mu. Model: Mu-4S. LV Configuration: Mu-4S M-4S-2.
  • Tansei 1 Nation: Japan. Payload: MS T1. Mass: 62 kg (136 lb). Class: Technology. Spacecraft: Tansei. Agency: ISAS. Perigee: 986 km (612 mi). Apogee: 1,106 km (687 mi). Inclination: 29.70 deg. Period: 106.10 min. COSPAR: 1971-011A. USAF Sat Cat: 4952. Engineering test for the launching of scientific satellites. Injection point 29.7 N, 145.8 E References: 2, 6.
1971 February 17 -
  • Management plans for Gagarin Cosmonaut Centre jeopardised. Nation: USSR. Management of TsPK is in question due to intrigues by Mishin and his allies within the VVS. After the death of Belyayev it was committed that Leonov would become head of the First Directorate of TsPK. This is now in doubt. References: 376.
1971 February 17 - Launch Site: Baikonur. Launch Complex: LC161/35. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1971 February 17 - 03:52 GMT - Launch Site: Vandenberg. Launch Complex: SLC10W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Burner 2. LV Configuration: Thor Burner 2 249.
  • DMSP Block 5A F3 Nation: USA. Program: DMSP. Payload: DAPP 3526. Mass: 195 kg (429 lb). Class: Earth. Type: Weather. Spacecraft: DMSP Block 5A. Agency: USAF. Perigee: 741 km (460 mi). Apogee: 799 km (496 mi). Inclination: 98.70 deg. Period: 100.20 min. COSPAR: 1971-012A. USAF Sat Cat: 4953. Defense Meteorological Satellite Program. References: 2, 6.
  • Calsphere 3A Nation: USA. Payload: NRL PL170A. Mass: 1.00 kg (2.20 lb). Class: Calibration. Spacecraft: Calsphere. Agency: NRL. Perigee: 509 km (316 mi). Apogee: 531 km (329 mi). Inclination: 98.40 deg. Period: 95.00 min. COSPAR: 1971-012C. USAF Sat Cat: 4957. Decay Date: 1989-10-17. Radar calibarion sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
  • Calsphere 4 Nation: USA. Payload: NRL PL170B. Mass: 1.00 kg (2.20 lb). Class: Calibration. Spacecraft: Calsphere. Agency: NRL. Perigee: 486 km (301 mi). Apogee: 502 km (311 mi). Inclination: 98.40 deg. Period: 94.50 min. COSPAR: 1971-012D. USAF Sat Cat: 4958. Decay Date: 1989-09-20. Radar calibarion sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
  • Calsphere 5 Nation: USA. Payload: NRL PL170C. Mass: 1.00 kg (2.20 lb). Class: Calibration. Spacecraft: Calsphere. Agency: NRL. Perigee: 340 km (210 mi). Apogee: 360 km (220 mi). Inclination: 98.20 deg. Period: 91.50 min. COSPAR: 1971-012E. USAF Sat Cat: 4963. Decay Date: 1990-01-07. Radar calibarion sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1971 February 17 - 07:25 GMT - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 3.
  • OLD FOX 05M demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1971 February 17 - 20:04 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 537 / Agena D 1659. FAILURE: Failure.
  • KH-4B 1113 Nation: USA. Payload: KH-4B s/n 1113. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4B. Agency: U.S. Air Force. COSPAR: F710217A. Decay Date: 1971-02-17. KH-4B. The launch vehicle had a very cold boattail due to a hose discovered to be leaking away warming air to the boattail. The boattail was colder than usual, below freezing. Based on earlier tests of the Thor for just that condition, as relayed by Ed Dierdorf, Thor chief engineer at the time, the temp low was of no concern.

    The only problem was that those tests were made with a Thor that carried a Rocketdyne engine lubricated with "lube oil". The Thor being launched used a fuel additive, "Orinite" (like STP "super snot"). The technician that pumped the Orinite into its cannister later stated, "It wasn't for lack of orinite. I put it in just like the procedure said, and I could feel when it was full (with the hand pump). To make sure, I gave it another slug."

    That "other slug" cracked the output valve that was only supposed to be cracked by turbopump output pressure. When it cracked the output valve a bit of the "honey" squirted down the tube toward engine bearing jets. This line had a low spot in it by design. The Orinite settled there. When it was chilled by the low temp air at lox loading, the Orinite formed a plug.

    Unaware of this chain of circumstances, Launch Director Philip Payne made the decision to launch. The rocket (carrying Agena D and payload) flew for 18 seconds, then wiped out its gears, causing the turbine to overspeed and shed its vanes. These punctured various parts in the boattail like machine gun bullets. With loss of power, the rocket fell not far from the launch pad into Bear Creek canyon.

    The final cause was therefore found to be loss of engine lubrication at startup. References: 126, 498.

  • SRV 825 Nation: USA. Payload: SRV 1113-1. Spacecraft: KH-4B. Agency: USAF. COSPAR: F710217B. References: 279.
  • SRV 826 Nation: USA. Payload: SRV 1113-2. Spacecraft: KH-4B. Agency: USAF. COSPAR: F710217C. References: 279.
1971 February 17 - 21:09 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53727-117.
  • Cosmos 395 Nation: USSR. Program: Tselina. Mass: 875 kg (1,929 lb). Class: Sigint. Spacecraft: Tselina-O. Agency: MO SSSR. Perigee: 529 km (328 mi). Apogee: 546 km (339 mi). Inclination: 74.00 deg. Period: 95.40 min. COSPAR: 1971-013A. USAF Sat Cat: 4955. Decay Date: 1980-04-06. Possible ELINT satellite. References: 2, 6.
1971 February 18 -
  • X-24 Flight 23 Nation: USA. Payload: X-24A flight 23. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Manke. Maximum Speed - 1606 kph. Maximum Altitude - 20544 m. Flight Time - 447 sec. References: 49, 97.
1971 February 18 - 13:59 GMT - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 396 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 285 km (177 mi). Inclination: 65.40 deg. Period: 89.40 min. COSPAR: 1971-014A. USAF Sat Cat: 4959. Duration: 13.00 days. Decay Date: 1971-03-03. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1971 February 19 -
  • Kamanin fascinated by peaceful use of nuclear explosives. Nation: USSR. The Minister of Medium Machine Building holds a conference on the occasion of the 53rd Anniversary of the Soviet Army. A film is shown on the use of nuclear explosives to extract oil in Central Asia - fantastic images. References: 376.
1971 February 20 - 03:23 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 4A. LV Configuration: Black Brant IVA AKF-4A-18.
  • Auroral emissions Aurora / ionosphere / plasma mission Nation: Canada. Agency: NRCC. Apogee: 785 km (487 mi). References: 2.
1971 February 22 - 00:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 350. LV Configuration: Aerobee 350 NASA 17.09UG.
  • Crab polarization X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 196 km (121 mi). References: 2.
1971 February 22 - 11:40 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC S85. FAILURE: Failure.
  • ESRO S85 Ultraviolet astronomy mission Nation: UK. Agency: BAC/ESRO. Apogee: 222 km (137 mi). References: 2.
1971 February 23 - Launch Site: Biscarosse. Launch Complex: -. Launch Pad: -. Launch Vehicle: Berenice. Model: Tibere.
  • ELECTRE Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 130 km (80 mi). References: 2.
1971 February 23 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • SSTTP M1-28 Target mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1971 February 24 -
  • VVS position to limit duration of DOS missions hopeless. Nation: USSR. Program: Salyut. Kutakhov calls Smirnov to give the VVS position on DOS-7K flights. He is told that Mishin has not only Ustinov and Smirnov, but even Brezhnev behind him in support of 30, and then 60 day spaceflight durations aboard DOS. The VVS' position of limiting flights to 20 to 24 days has no chance. References: 376.
1971 February 24 - 14:40 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.249NA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1971 February 25 - 01:13 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B.
  • Airglow Aeronomy mission Nation: USA. Agency: NRL. Apogee: 275 km (170 mi). References: 2.
1971 February 25 - 02:00 GMT - Launch Site: Vandenberg. Launch Complex: LF25. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • FOT GT102F Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1971 February 25 - 11:11 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
  • Cosmos 397 Nation: USSR. Mass: 1,400 kg (3,000 lb). Class: Military. Type: ASAT. Spacecraft: IS-A. Agency: PKO. Perigee: 572 km (355 mi). Apogee: 2,164 km (1,344 mi). Inclination: 65.70 deg. Period: 113.10 min. COSPAR: 1971-015A. USAF Sat Cat: 4964. ASAT interceptor. Intercept and destruction of target successful on second orbit. References: 2, 6, 272.
1971 February 26 -
  • M2 Flight 22 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 6. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Dana. Maximum Speed - 821 kph. Maximum Altitude - 13716 m. Flight Time - 348 sec. References: 49, 97.
1971 February 26 - 05:06 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511L.
  • Cosmos 398 Nation: USSR. Program: Lunar L3. Payload: Lunar Craft T2K no. 2. Mass: 5,500 kg (12,100 lb). Class: Manned. Type: Lunar lander. Spacecraft: LK. Agency: MOM. Perigee: 186 km (115 mi). Apogee: 1,958 km (1,216 mi). Inclination: 51.50 deg. Period: 106.70 min. COSPAR: 1971-016A. USAF Sat Cat: 4966. Duration: 8,463.78 days. Decay Date: 1995-12-10. Second space test of the LK moon lander test using the T2K version. Followed the same programme as Cosmos 379.
    Maneuver Summary:
    189km X 252km orbit to 186km X 1189km orbit. Delta V: 251 m/s
    186km X 1189km orbit to 200km X 10905km orbit. Delta V: 1320 m/s
    Total Delta V: 2832 m/s.
    Officially: Investigation of the upper atmosphere and outer space. References: 2, 6.
1971 February 26 - 10:18 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC S54. FAILURE: Failure.
  • ESRO S54 Solar x-ray mission Nation: Europe. Agency: ESRO. Apogee: 250 km (150 mi). References: 2.
1971 February 27 -
  • Mishin plans to get Almaz cancelled. Nation: USSR. Program: Almaz, Salyut. Spacecraft: Salyut 1, Almaz OPS, Spiral OS. Kamanin has a meeting scheduled with Chelomei, but this is cancelled and he is called to another meeting with Mishin -- all to advance Mishin's agenda. Mishin complains that he doesn't know what the Almaz project is about. He claims Chelomei has spent half a billion roubles so far, and has nothing to show for it. Mishin, on the other hand, has two DOS stations ready to fly, done at a cost of only 80 million roubles. But Kamanin knows very well who has really wasted hundreds of millions of roubles - Mishin. Mishin produces his plans for DOS#3 and DOS#4 follow-on stations. These are to be copies of Almaz, delivered in 18 months. Mishin says he is building ten 7K-S for the spacecraft, despite the fact that Karas at GUKOS is not interested in manned spaceflight. Afterwards Kamanin tells Kutakhov to warn Chelomei that he must support the VVS' 7K-S and Spiral projects, if he wants VVS support for Almaz. References: 376.
1971 February 27 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT80M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1971 February 28 - 07:53 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3. LV Configuration: Black Brant III AND-3-41.
  • Microwave background Submillimeter radio astronomy mission Nation: Canada. Agency: NRCC. Apogee: 152 km (94 mi). References: 2.
1971 March 1 -
  • X-24 Flight 24 Nation: USA. Payload: X-24A flight 24. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Powell. Maximum Speed - 1064 kph. Maximum Altitude - 17343 m. Flight Time - 437 sec. References: 49, 97.
1971 March 1 - Launch Vehicle: N1.
  • N1-L3 loses remaining priority Nation: USSR. Program: Lunar L3. Spacecraft: LK, Soyuz 7K-LOK. Flight: Apollo 13, Apollo 14. The Soviet leadership regained some interest in the N1-L3, after the near-tragedy of Apollo 13. It was felt that the Americans might cancel the remainder of the Apollo programme, leaving the road to the moon clear for the Soviet Union. However the successful flight of Apollo 14 redeemed the project, and the Central Committee lost all interest in the N1-L3. Additional Details: N1-L3 loses remaining priority. References: 367.
1971 March 1 - 09:15 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.22UG.
  • Astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1971 March 1 - 11:40 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 KP3.32.
  • Venus Lyra Alpha Ultraviolet astronomy mission Nation: USA. Agency: KPNO. Apogee: 160 km (90 mi). References: 2.
1971 March 2 - 1971 March 2 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • FOT GT92B-3 Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1971 March 2 - 10:08 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Cockatoo. LV Configuration: Cockatoo 110.
  • MPE Barium release? Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 218 km (135 mi). References: 2.
1971 March 2 - 10:33 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy/Ionosphere mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 March 2 - 10:38 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 SL922.
  • UK SL922 Ionosphere mission Nation: UK. Agency: BAC. Apogee: 223 km (138 mi). References: 2.
1971 March 2 - 21:14 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S16/2.
  • ESRO S16 / 2 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 143 km (88 mi). References: 2.
1971 March 3 -
  • Soviet of Chief Designers. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1, Soyuz 7KT-OK. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. DOS-7K #1 completed its factory testing on 3 March. Checkout at Baikonur is to be completed by 9 April, and launch is scheduled for 15 April. The first crew to the station will be launched aboard a Soyuz on 18-20 April. Remaining items to be cleared:
    • Vibration qualification test of the station test article are not complete. They will only begin on 5 March and will take two months using 3-shift work. Mishin wants the preliminary results on 20 March.
    • Four complete Igla systems are required. Five have been completed and are working satisfactorily.
    • The expiration date on the parachute installed in the Soyuz 10 capsule is 15 April. It will have to be repacked before the flight.
    • There were numerous failures in the first phase of environmental control system qualification tests. They have to be repaired before the second phase can even be started.
    • Mishin wants the first crew to stay on the station for 30 days, the second crew 45 days. Glushko and the doctors say this is a grave risk.
    References: 376.
1971 March 3 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Aero High. LV Configuration: Aero High AH5.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 178 km (110 mi). References: 2.
1971 March 3 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Aero High. LV Configuration: Aero High AH4.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 178 km (110 mi). References: 2.
1971 March 3 - 06:52 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB AAF-VB-32.
  • Electrons / ions Aurora mission Nation: Canada. Agency: NRCC. Apogee: 275 km (170 mi). References: 2.
1971 March 3 - 09:30 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 399 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 200 km (120 mi). Apogee: 285 km (177 mi). Inclination: 64.90 deg. Period: 89.30 min. COSPAR: 1971-017A. USAF Sat Cat: 5003. Duration: 14.00 days. Decay Date: 1971-03-17. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1971 March 3 - 12:15 GMT - Launch Site: Jiuquan. Launch Complex: LA2A. Launch Pad: -. Launch Vehicle: CZ-1. Model: CZ-1.
  • SJ-1 Nation: China. Payload: Shi Jian 1. Mass: 221 kg (487 lb). Class: Technology. Type: Comsat. Spacecraft: DFH-1. Agency: MAI. Perigee: 265 km (164 mi). Apogee: 1,833 km (1,138 mi). Inclination: 69.80 deg. Period: 106.10 min. COSPAR: 1971-018A. USAF Sat Cat: 5007. Decay Date: 1979-06-17. Similar in appearance to the American Telstar and conducted communications technology tests. References: 2, 6.
1971 March 4 - Launch Vehicle: N1, UR-700.
  • N1/L3 Expert Commission Nation: USSR. Program: Lunar L3. Spacecraft: Soyuz 7KT-OK, LK-700, Krechet. Pushkin and Kuznetsov brief Kamanin on the results of the N1/L3 expert commission. They found that the N1/L3 is unreliable and that the design needs to be fundamentally re-examined. Therefore the Soviet Ministers and Central Committee passed a decree that the commission must determine by 1 May 1971 what to do with the lunar project. Kamanin's opinion: abandon the N1-L3, modify Chelomei's UR-700 design to replace it, and design a new lunar landing spacecraft for missions in 1974-1975. Mishin is afraid of such a solution. Kamanin believes that the commission, headed by Keldysh, will finally recommend continued development and flight of Mishin's bad booster and even worse spacecraft. It is true that the N1 design has been substantially reworked in the last 18 months, but Kamanin believes it to be fundamentally flawed and that nothing can make it reliable.

    After Mishin pushed his Indian Ocean recovery plan for the L3, the VVS insisted on sea trials of the capsule. These showed the cosmonauts had to get out within 30 to 35 minutes before the valves to the interior started leaking seawater. The L3 is also unsafe due to the EVA method of transfer to the LK of a single unassisted cosmonaut. The Krechet spacesuit is very bulky and unmanoeuvrable.

    Prague wanted Gagarin's widow for International Women's Day.since Tereshkkova couldn't go, but she wants no part of public appearances. References: 376.

1971 March 5 -
  • Launch of DOS#1 is set for 15 April. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. Kamanin is still fighting the issue of mission length - he doesn't want to risk lives. Soyuz 9 landed virtually in the laps of the doctors, but what if they had made an emergency landing in the ocean, or taiga? They were in no condition to save themselves before assistance arrived. Every day over 20-22 days is a risk to the life of the crew, in Kamanin's view. Smirnov, Serbin, Mishin - they don't care about this.

    Meanwhile the doctor's verdict is in on Shonin. He is to be sent to a sanatorium for rehabilitation. References: 376.

1971 March 5 - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: LC43/pad?. Launch Vehicle: Soyuz. Model: Voskhod 11A57. FAILURE: Failure.
  • Zenit-2M Nation: USSR. Spacecraft: Zenit-2M. Agency: RVSN. COSPAR: F710305A. Area survey photo reconnaissance satellite. References: 279.
1971 March 5 - 08:15 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/4. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. FAILURE: Second stage failed 133 seconds after launch.
  • DS-P1-Yu s/n 39 Nation: USSR. Program: DS. Payload: DS-P1-Yu. Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: RVSN. COSPAR: F710305B. Development of systems for air defence and the control of outer space. References: 2.
1971 March 6 -
  • Space Plan for 1971 unrealistic. Nation: USSR. Program: Salyut, Almaz. Spacecraft: Salyut 1, Almaz OPS, TKS, Spiral OS. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. The space plan for 1971 has finally been approved. There are to be three space stations launched, manned by ten Soyuz launches and a total of over 12 different crewmembers in space during the year. But it is clear to Kamanin that the second DOS and first Almaz station will not really be ready this year. And there won't be more than two Soyuz and two TKS transports available by the end of the year. Ranazomov says that Chelomei's TKS, being designed to fly to the Almaz, will cover many of he same requirements of the Spiral spaceplane. He proposes that Mikoyan should collaborate with Chelomei on Spiral. Meanwhile simulators at TsPK remain underfunded. References: 376.
1971 March 8 - 11:38 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. FAILURE: Failure.
  • Caribou V Aurora ultraviolet mission Nation: USA. Agency: Sandia. Apogee: 0 km ( mi). References: 2.
1971 March 9 -
  • Major DOS training exercise by first crew. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. A major training session is held with Shatalov, Yeliseyev, and Rukavishnikov. They make a 15 hour simulated 'flight' aboard the DOS trainer from 09:15 to 22:45. All operations expected in a thirty-day mission to the station are gone through. This includes simulation of emergencies to test the reactions of both the crew and ground controllers. Kamanin receives a letter from Anders, thanking him for the tour of Star City. Representatives from the Swedish firm are in town to negotiate the contract for the TsF-18 18-metre radius centrifuge. Both Korolev and Mishin fought against the VVS getting such a centrifuge. References: 376.
1971 March 10 - 17:38 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.382GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 113 km (70 mi). References: 2.
1971 March 10 - 17:59 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.478UM.
  • UM Pitot 53 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 179 km (111 mi). References: 2.
1971 March 10 - 18:26 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.479UM.
  • UM Pitot 54 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 181 km (112 mi). References: 2.
1971 March 10 - 18:41 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.480UM.
  • UM Pitot 55 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 171 km (106 mi). References: 2.
1971 March 10 - 19:11 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.383GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 113 km (70 mi). References: 2.
1971 March 11 - 1971 March 11 - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena B035.
  • Re-entry Vehicle test Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1971 March 11 - 08:56 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC S55.
  • ESRO S55 X-ray astronomy mission Nation: Europe. Agency: ESRO. Apogee: 159 km (98 mi). References: 2.
1971 March 11 - 10:37 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk Caribou V.
  • Aurora ultraviolet mission Nation: USA. Agency: Sandia. Apogee: 270 km (160 mi). References: 2.
1971 March 12 - 04:13 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.015-3.
  • Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 280 km (170 mi). References: 2.
1971 March 12 - 06:55 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.913-3.
  • Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 283 km (175 mi). References: 2.
1971 March 12 - 21:49 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P69K.
  • Auroral electrons Aurora mission Nation: UK. Agency: SRC. Apogee: 153 km (95 mi). References: 2.
1971 March 13 - 00:50 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.388UA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1971 March 13 - 16:15 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 March 13 - 16:15 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta M6. LV Configuration: Thor Delta M6 562/D83.
  • Explorer 43 Nation: USA. Program: Explorer. Payload: IMP I. Mass: 288 kg (634 lb). Class: Earth. Type: Magnetosphere. Spacecraft: IMP. Agency: NASA GSF. Perigee: 1,845 km (1,146 mi). Apogee: 203,130 km (126,210 mi). Inclination: 31.20 deg. Period: 5,957.90 min. COSPAR: 1971-019A. USAF Sat Cat: 5043. Decay Date: 1974-10-02. Earth magnetosphere research. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1971 March 13 - 22:55 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 March 14 - 16:25 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Ionosphere mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 March 15 -
  • Major DOS training exercise by third crew. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. The third, back-up DOS crew of Dobrovolsky, Volkov and Patsayev train in the DOS trainer. All of the crews have made good runs, with no mistakes or failures. Shatalov, after training on the DOS simulator, now supports Mishin's 30 day flight approach. He has also talked to Yeliseyev and Sevastyanov about the matter. He believes there may be a very different reaction to zero-G from individual to individual, and the Soyuz 9 crew may have been the wrong two individuals. References: 376.
1971 March 15 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. Model: UR-100K.
  • Last State trials launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 15 - Launch Site: Hall Beach. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.126GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 March 15 - Launch Site: Cape Parry. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.122GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 March 15 - 17:55 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S87/1.
  • ESRO S87 / 1 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 188 km (116 mi). References: 2.
1971 March 15 - 18:17 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 March 15 - 23:00 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3E-39.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1971 March 16 - 09:05 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.14UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 March 16 - 19:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 CRL A04.002-2.
  • Extreme ultraviolet Solar extreme ultraviolet mission Nation: USA. Agency: AFCRL. Apogee: 270 km (160 mi). References: 2.
1971 March 17 - 1971 March 17 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • SSTTP M1-13 Target mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1971 March 17 - 10:57 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.95UA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 March 17 - 16:55 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 March 18 - Launch Site: Hall Beach. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.127GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 March 18 - 17:10 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 March 18 - 19:39 GMT - Launch Site: Kourou. Launch Complex: ALFS. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.380GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 125 km (77 mi). References: 2.
1971 March 18 - 21:45 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65027-118.
  • Cosmos 400 Nation: USSR. Payload: DS-P1-M s/n 3. Mass: 650 kg (1,430 lb). Class: Military. Type: ASAT Target. Spacecraft: DS-P1-M. Agency: MO SSSR. Perigee: 990 km (610 mi). Apogee: 995 km (618 mi). Inclination: 65.80 deg. Period: 105.00 min. COSPAR: 1971-020A. USAF Sat Cat: 5050. Completed Operations Date: 1972-08-22. ASAT target for Cosmos 404 interceptor. References: 2, 6, 99, 272.
1971 March 19 -
  • State Commission for Launch of DOS#1. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. The VVS insists that the Soyuz 10 crew land in daylight. Mishin says that in order that the crew can land in daylight at the end of the 30-day mission, the spacecraft must be launched at 03:00 at night. Kamanin believes this also to be unsafe. References: 376.
1971 March 19 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 19 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 19 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 19 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 19 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 19 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 19 - Launch Site: Hall Beach. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.123GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 March 19 - Launch Site: Hall Beach. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.128GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 250 km (150 mi). References: 2.
1971 March 19 - 12:05 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.94UA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 March 19 - 12:38 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk.
  • Ionosphere / aurora mission Nation: USA. Agency: Sandia. Apogee: 270 km (160 mi). References: 2.
1971 March 20 -
  • DOS crews arrives in Baikonur. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. Shatalov's crew arrived at 09:00 aboard a Tu-104 and were ensconced in Room 14 of the Hotel Kosmonavt. Two further Tu-104's arrived 20 and 30 minutes later with the second and third crews. At 18:00 they all went to the MIK assembly hall to view the two Soyuz spacecraft and the station. There were electrical problems with the station, and they finally returned to the hotel at 24:00 without the problem having been resolved. Kamanin notes two films are to be screened tomorrow - a Bulgarian movie and the Soviet film 'Diplomat'. References: 376.
1971 March 20 - Launch Site: Hall Beach. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.124GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 March 20 - 05:30 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.21UG. FAILURE: Failure.
  • X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1971 March 20 - 05:42 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk CRL A08.019-1.
  • Aurora mission Nation: USA. Agency: AFCRL. Apogee: 336 km (208 mi). References: 2.
1971 March 20 - 05:44 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.019-2.
  • Aurora mission Nation: USA. Agency: AFCRL. Apogee: 164 km (101 mi). References: 2.
1971 March 20 - 07:53 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II AHF-2-115.
  • Auroral VUV Test / aurora / ionosphere mission Nation: Canada. Agency: NRCC. Apogee: 151 km (93 mi). References: 2.
1971 March 20 - 08:15 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.17UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 March 21 -
  • DOS communications tests at Baikonur Nation: USSR. Program: Salyut. Spacecraft: Salyut 1, Penguin. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. Due to problems with the electrical system aboard the station, the crews are unable to start their training aboard the actual station until 22:00. So after breakfast they work on their flight plans and logs and test the training suits to be used on this flight for the first time. This includes the Penguin suit which has elastic bands sewn into it to simulate the strain of gravity. At 17:00 the crews go to the MIK and start communications tests on the DOS. All proceeds normally. On the bus back, the crews discuss the new tracking ship Yuri Gagarin. It has a displacement of 45,000 tonnes and cost 120 million roubles. It will expand the time communications are possible with the ground during the long station flight. References: 376.
1971 March 21 - Launch Site: Hall Beach. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.125GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1971 March 21 - 03:45 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 33B. LV Configuration: Titan 33B 33B-1 (3B-36) / Ascent Agena D.
  • Jumpseat 1 Nation: USA. Mass: 700 kg (1,540 lb). Class: Sigint. Spacecraft: Jumpseat. Agency: NRO/USAF. Perigee: 390 km (240 mi). Apogee: 33,800 km (21,000 mi). Inclination: 63.20 deg. Period: 596.70 min. COSPAR: 1971-021A. USAF Sat Cat: 5053. References: 2, 6.
1971 March 22 -
  • Problems with Igla system on DOS. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. There are problems with the Igla rendezvous system and also the stabilisation systems aboard DOS#1. The April 15 launch date is not realistic, according to Shabarov's deputies, although he himself says he can still meet the schedule. From 12:00 to 16:00 the cosmonauts participate in communications tests between the Soyuz spacecraft and the station. They go all right, but there are many problems with the ground segment. Mishin arrives in the evening. He has to give the VPK the final word on 27 March as to the launch date for the station. Shabarov is afraid to tell Mishin about the problems they are having with the Igla system. References: 376.
1971 March 22 - Launch Site: Thule AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Sparrow Arcas. LV Configuration: Sparrow Arcas PCA.
  • Ionosphere mission Nation: USA. Agency: AFCRL. Apogee: 112 km (69 mi). References: 2.
1971 March 22 - 16:50 GMT - Launch Site: Hall Beach. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.129GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 265 km (164 mi). References: 2.
1971 March 23 -
  • Cosmonauts return to Moscow from Tyuratam. Nation: USSR. Program: Salyut. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. A four-story school burned down the previous night in Leninsk. The cosmonauts and space centre technicians watched the USA-USSR ice hockey match, which went from 23:00 until 02:00 the next morning. Kamanin returns to Moscow aboard a Tu-104. Aboard the flight the political intrigues surrounding selection of Kamanin's deputy are discussed. References: 376.
1971 March 24 -
  • Gagarin film Nation: USSR. Gagarin Centre management are away at various sites. Kamanin enjoys the television film on Gagarin, 'About my friend', broadcast from Leningrad. References: 376.
1971 March 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 24 - 05:26 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5C. LV Configuration: Black Brant VC CRL A18.006-3.
  • Airglow / Auroral infrared Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 366 km (227 mi). References: 2.
1971 March 24 - 07:25 GMT - Launch Site: Vandenberg. Launch Complex: LF08. Launch Pad: -. Launch Vehicle: Minuteman 3.
  • OT GT01GM operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1971 March 24 - 18:32 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S87/2.
  • ESRO S87 / 2 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 190 km (110 mi). References: 2.
1971 March 24 - 21:05 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 538 / Agena D 1660.
  • KH-4B 1114 Nation: USA. Payload: KH-4B s/n 1114 / Agena D 1660. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4B. Agency: NRO/CIA. Perigee: 156 km (96 mi). Apogee: 245 km (152 mi). Inclination: 81.50 deg. Period: 88.40 min. COSPAR: 1971-022A. USAF Sat Cat: 5059. Decay Date: 1971-04-12. KH-4B. The overall image quality is good and comparable to the best of past missions. On-board program failed References: 2, 6.
1971 March 25 -
  • DOS#1 Launch Commission. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. The launch date, time, and first mission duration are debated. The VVS specialists now say a night landing by a Soyuz is acceptable from a safety point of view. Only two months earlier they were rejecting the possibility - these are people without principles, in Kamanin's view. He believes the crew's lives will be at risk with the planned thirty day flight duration. References: 376.
1971 March 25 - 13:50 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C S56B/1. FAILURE: Failure.
  • ESRO S56B / 1 Ionosphere / solar ultraviolet / x-ray mission Nation: Europe. Agency: ESRO. Apogee: 130 km (80 mi). References: 2.
1971 March 26 - Launch Vehicle: Soyuz. Model: Soyuz 11A511.
  • Yantar-1FKT development authorised. Nation: USSR. Spacecraft: Yantar-1KFT. Central Committee of the Communist Party and Council of Soviet Ministers Decree 182-63 'On development of the Yantar-1KFT reconnaissance and cartographic satellite and the 11A511K launcher' was issued. References: 474.
1971 March 26 -
  • VPK meets at the Kremlin. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. The launch of DOS#1 is set for 15-20 April. The first crew will launch three days later on a thirty-day mission. 25 days after they return to earth the second crew will be launched. That crew will stay aboard for 30 to 45 days. The spaceships and crews are declared ready for both missions. References: 376.
1971 March 26 - Launch Vehicle: Shuttle.
  • Shuttle Phase B Final Reports Nation: USA. Taking into account NASA and USAF comments on the draft proposals, and specification revisions, the teams of McDonnell Douglas/Martin Marrietta and North American Rockwell/General Dynamics made their final proposals under shuttle Phase B contracts. Based on the strict specifications of NASA, the low cross-range and high-cross range versions of the orbiter stages were similar. The associate contractors provided considerably different winged booster stage designs. One common feature was the use of aluminium structures and non-metallic thermal protection systems. In late 1969 the USAF had indicated a preference for all-aluminium structures in the shuttle due to a titanium shortage. This requirement forced a move to non-metallic thermal protection systems, which at the time it was thought would weigh 15% less but cost 300% more. Thermal protection shingles for a titanium structure would weigh 2300 to 4500 kg less, but an aluminium structure would weight about 1800 kg more - meaning there was no essential weight difference between the two approaches. Therefore at the aluminium structure was accepted as a specification requirement. In retrospect it could hardly have been necessary to apply this requirement on a project where only a few flight vehicles were be built. It made the shuttle much more vulnerable to any breach of heat shield integrity and would lead to the death of the Columbia crew 35 years later. The resulting need for a non-metallic thermal protection system would also have enormous cost and schedule consequences for the actual program. References: 44.
1971 March 26 - 15:06 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.
1971 March 27 -
  • Gagarin exhibit at Space City Museum. Nation: USSR. t is three years since Gagarin's death. Exhibits at the space centre museum commemorating the cosmonaut include Vostok spacecraft and MiG-15UTI aircraft of the types he flew; three automobiles he owned; films, etc. References: 376.
1971 March 27 - 02:44 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NRL NB3.245.
  • Astronomy mission Nation: USA. Agency: NRL. Apogee: 200 km (120 mi). References: 2.
1971 March 27 - 10:59 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 401 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 185 km (114 mi). Apogee: 290 km (180 mi). Inclination: 72.80 deg. Period: 89.30 min. COSPAR: 1971-023A. USAF Sat Cat: 5086. Duration: 13.00 days. Decay Date: 1971-04-09. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1971 March 27 - 12:26 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk.
  • Ionosphere / aurora mission Nation: USA. Agency: Sandia. Apogee: 270 km (160 mi). References: 2.
1971 March 28 - 19:42 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Ionosphere mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 March 29 -
  • X-24 Flight 25 Nation: USA. Payload: X-24A flight 25. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Manke. Fastest X-24 flight. Maximum Speed - 1667 kph. Maximum Altitude - 21488 m. Flight Time - 446 sec. References: 49, 97.
1971 March 29 -
  • VVS crashes up. Nation: USSR. Kamanin notes that it was a bad safety month for the VVS. Ten aircraft were lost, six of those in three midair collisions (two MiG-21's in Egypt, two MiG-17's in Khabarovsk, and two helicopters in Tashkent). There were 29 losses in the first four months of 1971 (compared to 18 in 1970). Kamanin sees this as symptomatic of Kutakhov's poor management. References: 376.
1971 March 29 - 08:45 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Ionosphere mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 March 29 - 20:10 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Apogee: 150 km (90 mi). References: 2.
1971 March 29 - 23:05 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3E-12.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1971 March 30 -
  • 24th Congress of he Communist Party of the Soviet Union Nation: USSR. The Congress began in the Kremlin at 10:00. Vital questions concerning the future space program will be considered. References: 376.
1971 March 30 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 30 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 30 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 30 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 30 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 30 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 30 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1971 March 31 -
  • Cosmonaut delegates to Communist Party Congress. Nation: USSR. The Communist Party Congress is addressed for five hours by Brezhnev. There are 5,000 delegates, including 101 international delegations from 90 countries. Brezhnev promises that the imperialist lackeys will be wiped out one by one until communism triumphs over the whole planet. Five cosmonauts are delegates - Nikolayev, Beregovoi, Shatalov, Yeliseyev, and Tereshkova. References: 376.

PreviousHomeNext


Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2008 except where otherwise noted.