1972 October 1 - Launch Site: White Sea Launch Area. Launch Complex: -. Launch Pad: 65.5 N x 38.0 E. Launch Vehicle: R-29. Model: Vysota. -
Test mission Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E. References: 2.
1972 October 1 - Launch Site: Sea-launched. Launch Complex: -. Launch Pad: UNKPL. Launch Vehicle: R-27. Model: Zyb. LV Configuration: Zyb-Mod 2. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi). References: 2.
1972 October 2 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. -
Last of two Atlas/Burner II space launches Nation: USA. Last of two Atlas/Burner II space launches from Vandenberg AFB (first launch on 16 August 1968). References: 88.
1972 October 2 - 20:09 GMT - Launch Site: Vandenberg. Launch Complex: 576A1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Burner 2A. LV Configuration: Atlas / Burner 2A 102F. -
RADCAT Nation: USA. Payload: Radsat / Radcat. Mass: 208 kg (458 lb). Class: Technology. Type: Military. Spacecraft: RADCAT. Agency: USA. Perigee: 627 km (389 mi). Apogee: 638 km (396 mi). Inclination: 98.60 deg. Period: 97.40 min. COSPAR: 1972-076A. USAF Sat Cat: 6212. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
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Radsat Nation: USA. Payload: P 72-1. Mass: 726 kg (1,600 lb). Class: Technology. Type: Military. Spacecraft: Radsat. Agency: USAF. Perigee: 688 km (427 mi). Apogee: 705 km (438 mi). Inclination: 98.70 deg. Period: 98.70 min. COSPAR: 1972-076B. USAF Sat Cat: 6217. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
1972 October 3 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2. -
FOT GT109M Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1972 October 4 - 12:00 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 522 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 212 km (131 mi). Apogee: 309 km (192 mi). Inclination: 72.00 deg. Period: 89.70 min. COSPAR: 1972-077A. USAF Sat Cat: 6219. Duration: 13.00 days. Decay Date: 1972-10-17. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1972 October 5 - -
M2 Flight 35 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 19. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Dana. Maximum Speed - 1455 kph. Maximum Altitude - 20210 m. Flight Time - 376 sec. References: 49, 97.
1972 October 5 - 11:30 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 523 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 63. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 271 km (168 mi). Apogee: 478 km (297 mi). Inclination: 71.00 deg. Period: 92.00 min. COSPAR: 1972-078A. USAF Sat Cat: 6222. Completed Operations Date: 1973-02-21. Decay Date: 1973-03-07. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1972 October 5 - 15:00 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3T. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1972 October 5 - 19:24 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P127A. -
Particles / substorm Aurora mission Nation: UK. Agency: SRC. Apogee: 117 km (72 mi). References: 2.
1972 October 7 - 22:47 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P42A. -
Particles / substorm Aurora mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1972 October 8 - 16:10 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.499UA. -
SSC NNA 3 Meteorites mission Nation: Sweden. Agency: NASA/SSC. Apogee: 109 km (67 mi). References: 2.
1972 October 9 - 12:51 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Sandhawk Tomahawk. LV Configuration: Sandhawk Tomahawk Sandia 152-191. -
Ba CHACHALACA Aeronomy / Fields mission Nation: USA. Agency: Sandia. Apogee: 500 km (310 mi). References: 2.
1972 October 9 - 15:30 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.501UA. -
SSC NNA 4 Meteorites mission Nation: Sweden. Agency: NASA/SSC. Apogee: 109 km (67 mi). References: 2.
1972 October 10 - 14:00 GMT - Launch Site: Biscarosse. Launch Complex: -. Launch Pad: -. Launch Vehicle: Forschungsflugkorper. LV Configuration: Forschungsflugkorper 1. FAILURE: Failure. -
DLR C-FFK-45 test Nation: Germany. Agency: DLR. Apogee: 0 km ( mi). References: 2.
1972 October 10 - 18:03 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3D. LV Configuration: Titan IIID 23D-3. -
KH-9 no. 04 Nation: USA. Mass: 13,300 kg (29,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-9. Agency: NRO/CIA. Perigee: 160 km (90 mi). Apogee: 281 km (174 mi). Inclination: 96.50 deg. Period: 88.90 min. COSPAR: 1972-079A. USAF Sat Cat: 6227. Decay Date: 1973-01-08. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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OPS 8314/2 Nation: USA. Payload: SSF-C No. 3. Mass: 60 kg (132 lb). Class: Sigint. Spacecraft: SSF. Agency: NRO/USAF. Perigee: 1,420 km (880 mi). Apogee: 1,464 km (909 mi). Inclination: 95.60 deg. Period: 114.70 min. COSPAR: 1972-079C. USAF Sat Cat: 6822. ABM monitoring. References: 2, 6, 172.
1972 October 10 - 21:21 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P55A. -
VLF radio hiss Aurora mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1972 October 11 - 03:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA NRL NF9.250. -
Auroral infrared Aurora mission Nation: USA. Agency: NRL. Apogee: 144 km (89 mi). References: 2.
1972 October 11 - 11:30 GMT - Launch Site: Vandenberg. Launch Complex: 395-C. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-78. -
Operational Test M2-14 Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). SSTTP M2-14 Target mission References: 2.
1972 October 11 - 11:31 GMT - Launch Site: Vandenberg. Launch Complex: PLC-C. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 CRL A04.116-4. -
CHASER ABM infrared sensor technology mission Nation: USA. Agency: AFCRL. Apogee: 151 km (93 mi). References: 2.
1972 October 11 - 13:13 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Sandhawk Tomahawk. LV Configuration: Sandhawk Tomahawk Sandia 152-192. FAILURE: Failure. -
Barium release FAISON Aeronomy / Fields mission Nation: USA. Agency: Sandia. Apogee: 0 km ( mi). References: 2.
1972 October 11 - 13:19 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 524 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 49. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 266 km (165 mi). Apogee: 510 km (310 mi). Inclination: 70.00 deg. Period: 92.30 min. COSPAR: 1972-080A. USAF Sat Cat: 6229. Completed Operations Date: 1973-03-25. Decay Date: 1973-03-25. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1972 October 12 - 15:33 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.502UA. -
SSC NNA 5 Meteorites mission Nation: Sweden. Agency: NASA/SSC. Apogee: 109 km (67 mi). References: 2.
1972 October 13 - 00:28 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S105. -
ESRO S105 Auroral mission Nation: Europe. Agency: ESRO. Apogee: 207 km (128 mi). References: 2.
1972 October 13 - 15:11 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.504CA. -
Lithium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 160 km (90 mi). References: 2.
1972 October 13 - 16:39 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.505CA. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 160 km (90 mi). References: 2.
1972 October 13 - 18:57 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure 2A. LV Configuration: Centaure 2A ISRO 5.17. -
ISRO 5.17 Fields mission Nation: India. Agency: ISRO. Apogee: 120 km (70 mi). References: 2.
1972 October 14 - Launch Vehicle: N1. -
Electrical trials of the N1 7L were successfully completed. Nation: USSR. Program: Lunar L3. References: 367.
1972 October 14 - 06:16 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. -
Molniya 1-21 Nation: USSR. Program: Molniya. Payload: Molniya-1. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-1. Agency: MOM. Perigee: 494 km (306 mi). Apogee: 34,684 km (21,551 mi). Inclination: 65.40 deg. Period: 615.40 min. COSPAR: 1972-081A. USAF Sat Cat: 6231. Decay Date: 1977-11-01. Uncertain if Molniya-1T model was Molniya-1 or Molniya-1T. Operation of the long-range telephone and telegraph radiocommunications system in the USSR; transmission of television programmes to stations in the Orbita network. References: 2, 6.
1972 October 15 - 15:00 GMT - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Strypi. Model: Strypi VIIAR. LV Configuration: Strypi VIIAR NASA 12.18NE. -
RCTV / Art. Aurora Test / electron gun mission Nation: USA. Agency: NASA. Apogee: 500 km (310 mi). References: 2.
1972 October 15 - 17:19 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 0300. LV Configuration: Delta 0300 575/D91. -
NOAA 2 Nation: USA. Program: Tiros. Payload: ITOS D. Mass: 344 kg (758 lb). Class: Earth. Type: Weather. Spacecraft: ITOS. Agency: NOAA. Perigee: 1,449 km (900 mi). Apogee: 1,455 km (904 mi). Inclination: 101.80 deg. Period: 114.90 min. COSPAR: 1972-082A. USAF Sat Cat: 6235. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 2, 6.
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Oscar 6 Nation: USA. Program: Oscar. Payload: Amsat-Oscar-6. Mass: 16 kg (35 lb). Class: Communications. Type: Amateur Radio. Spacecraft: Oscar. Agency: AMSAT-NA. Perigee: 1,449 km (900 mi). Apogee: 1,455 km (904 mi). Inclination: 101.70 deg. Period: 114.90 min. COSPAR: 1972-082B. USAF Sat Cat: 6236. AMSAT-OSCAR 6 was launched piggyback with ITOS-D (NOAA 2). AO-6 was the first phase 2 satellite (Phase II-A). Weight 16 kg. Box shaped 430 x 300 x 150 mm. Quarter-wave monopole antennas (144 and 435 MHz) and half-wave dipole antenna (29 MHz). Firsts: complex control system using discrete logic; satellite-to-satellite relay communication via AO-7; demonstrated doppler-location of ground station for search and rescue; demonstrated low-cost medical data relay from remote locations. Equipped with solar panels powering NiCd batteries, AO-6 provided 24 V at 3.5 W power to three transponders. It carried a Mode A transponder (100 kHz wide at 1 W) and provided store-and-forward morse and teletype messages (named Codestore) for later transmission. AO-6 lasted 4.5 years until a battery failure ceased operation on June 21, 1977. Subsystems were built in the United States, Australia, and Germany.
References: 2, 6.
1972 October 16 - Launch Site: Vandenberg. Launch Complex: LF25. Launch Pad: -. Launch Vehicle: Minuteman 3. -
OT GT17GB operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1972 October 17 - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M Yu149-40. FAILURE: Launch vehicle failed to orbit - unknown cause.
1972 October 17 - 18:39 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 SL1022. -
Composition / scattering Ionosphere mission Nation: UK. Agency: BAC. Apogee: 142 km (88 mi). References: 2.
1972 October 18 - Launch Vehicle: Proton. Model: Proton 8K82K / 11S824. -
UR-500K failure investigation. Nation: USSR. Afanasyev was back at the cosmodrome for investigation of the latest UR-500K failure. References: 367.
1972 October 18 - 11:59 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 525 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 207 km (128 mi). Apogee: 268 km (166 mi). Inclination: 65.00 deg. Period: 89.20 min. COSPAR: 1972-083A. USAF Sat Cat: 6248. Duration: 11.00 days. Decay Date: 1972-10-29. Area survey photo reconnaissance satellite; returned film capsule; separated Nauka autonomous subsatellite 16KS No 161 / 1L which tested Kondor control system for Yantar satellite. References: 2, 6, 69.
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Nauka Cosmos 525 Nation: USSR. Payload: Nauka 16KS No. 1L. Spacecraft: Nauka. Agency: MOM. Perigee: 191 km (118 mi). Apogee: 258 km (160 mi). Inclination: 65.30 deg. Period: 88.99 min. COSPAR: 1972-083C. USAF Sat Cat: 6258. Decay Date: 1972-11-01. References: 2, 279.
1972 October 19 - -
M2 Flight 36 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 20. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Manke. Maximum Speed - 961 kph. Maximum Altitude - 14360 m. Flight Time - 359 sec. References: 49, 97.
1972 October 19 - Launch Site: Baikonur. Launch Complex: LC104. Launch Pad: -. Launch Vehicle: R-36M. FAILURE: Failure. -
BI-4 Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1972 October 20 - 09:05 GMT - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 2. -
FOT GT110M Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1972 October 20 - 12:17 GMT - Launch Site: Barking Sands. Launch Complex: LC14. Launch Pad: -. Launch Vehicle: Sandhawk. Model: Terrier Sandhawk. LV Configuration: Terrier Sandhawk Sandia 281-29. -
LRL ACS-4D X-ray astronomy mission Nation: USA. Agency: Sandia. Apogee: 310 km (190 mi). References: 2.
1972 October 21 - 12:34 GMT - Launch Site: Barking Sands. Launch Complex: LC12. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. LV Configuration: Terrier Tomahawk Sandia 152-197. -
LRL ACS-7B X-ray astronomy mission Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi). References: 2.
1972 October 21 - 13:16 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.151UE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1972 October 21 - 20:00 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P126A. -
Particles / substorm Aurora mission Nation: UK. Agency: SRC. Apogee: 117 km (72 mi). References: 2.
1972 October 23 - 11:51 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 6 AC. LV Configuration: Skylark 6 AC SL402. -
Soft X-ray / Lunar ultraviolet X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 210 km (130 mi). References: 2.
1972 October 23 - 19:05 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P125A. -
Electron analyser Aurora mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1972 October 24 - 15:00 GMT - Launch Site: Biscarosse. Launch Complex: -. Launch Pad: -. Launch Vehicle: Forschungsflugkorper. LV Configuration: Forschungsflugkorper 2. FAILURE: Failure. -
DLR C-FFK-46 test Nation: Germany. Agency: DLR. Apogee: 0 km ( mi). References: 2.
1972 October 24 - 17:20 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB NASA 21.20GT. -
CALROC test Nation: USA. Agency: NASA. Apogee: 282 km (175 mi). References: 2.
1972 October 25 - 10:39 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 526 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 61. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 274 km (170 mi). Apogee: 485 km (301 mi). Inclination: 70.00 deg. Period: 92.10 min. COSPAR: 1972-084A. USAF Sat Cat: 6254. Completed Operations Date: 1973-04-06. Decay Date: 1973-04-08. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1972 October 25 - 13:22 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 160 km (90 mi). References: 2.
1972 October 26 - Launch Site: Kwajalein. Launch Complex: Meck. Launch Pad: -. Launch Vehicle: Spartan. LV Configuration: Spartan ABM 800037. -
Safeguard M2-12 Interceptor mission Nation: USA. Agency: USA. Apogee: 100 km (60 mi). References: 2.
1972 October 26 - 04:30 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL1003. -
X-ray BCS / RMC Solar x-ray mission Nation: UK. Agency: BAC. Apogee: 195 km (121 mi). References: 2.
1972 October 26 - 11:00 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 170 km (100 mi). References: 2.
1972 October 26 - 22:05 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M. -
Meteor 1-13 Nation: USSR. Payload: Meteor M no. 13. Mass: 3,800 kg (8,300 lb). Class: Earth. Type: Weather. Spacecraft: Meteor M. Agency: MOM. Perigee: 851 km (528 mi). Apogee: 880 km (540 mi). Inclination: 81.20 deg. Period: 102.30 min. COSPAR: 1972-085A. USAF Sat Cat: 6256. Investigation of the upper atmosphere and outer space. References: 2, 6.
1972 October 27 - Launch Site: Green River. Launch Complex: -. Launch Pad: -. Launch Vehicle: Athena RTV. Model: Athena H. LV Configuration: Athena H H007. -
ABC-2 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1972 October 27 - 23:02 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 170 km (100 mi). References: 2.
1972 October 28 - 03:23 GMT - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. -
HK-1 Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1972 October 30 - 17:45 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.67US. -
Solar mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1972 October 31 - 02:42 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 165 km (102 mi). References: 2.
1972 October 31 - 10:30 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 120 km (70 mi). References: 2.
1972 October 31 - 13:29 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 527 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 207 km (128 mi). Apogee: 306 km (190 mi). Inclination: 65.40 deg. Period: 89.60 min. COSPAR: 1972-086A. USAF Sat Cat: 6260. Duration: 13.00 days. Decay Date: 1972-11-13. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1972 October 31 - 23:32 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.106-1. -
Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 170 km (100 mi). References: 2.
1972 October 31 - 23:51 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.105-6. -
Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 192 km (119 mi). References: 2.
1972 November 1 - -
M2 Flight 37 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 21. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Manke. Maximum Speed - 1292 kph. Maximum Altitude - 21730 m. Flight Time - 378 sec. References: 49, 97.
1972 November 1 - 01:04 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.105-5. -
Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 174 km (108 mi). References: 2.
1972 November 1 - 01:30 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.105-4. -
Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 203 km (126 mi). References: 2.
1972 November 1 - 02:08 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M Yu149-46. -
Cosmos 528 Nation: USSR. Program: Strela. Payload: Strela-1M no. 33. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,367 km (849 mi). Apogee: 1,467 km (911 mi). Inclination: 74.00 deg. Period: 114.20 min. COSPAR: 1972-087A. USAF Sat Cat: 6262. Eight satellites launched by a single carrier rocket. References: 2, 6.
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Cosmos 529 Nation: USSR. Program: Strela. Payload: Strela-1M no. 34. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,402 km (871 mi). Apogee: 1,468 km (912 mi). Inclination: 74.00 deg. Period: 114.60 min. COSPAR: 1972-087B. USAF Sat Cat: 6264. References: 2, 6.
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Cosmos 530 Nation: USSR. Program: Strela. Payload: Strela-1M no. 35. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,333 km (828 mi). Apogee: 1,468 km (912 mi). Inclination: 74.00 deg. Period: 113.80 min. COSPAR: 1972-087C. USAF Sat Cat: 6265. References: 2, 6.
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Cosmos 531 Nation: USSR. Program: Strela. Payload: Strela-1M no. 36. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,421 km (882 mi). Apogee: 1,469 km (912 mi). Inclination: 74.00 deg. Period: 114.80 min. COSPAR: 1972-087D. USAF Sat Cat: 6266. References: 2, 6.
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Cosmos 532 Nation: USSR. Program: Strela. Payload: Strela-1M no. 37. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,300 km (800 mi). Apogee: 1,467 km (911 mi). Inclination: 74.00 deg. Period: 113.40 min. COSPAR: 1972-087E. USAF Sat Cat: 6267. References: 2, 6.
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Cosmos 533 Nation: USSR. Program: Strela. Payload: Strela-1M no. 38. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,317 km (818 mi). Apogee: 1,468 km (912 mi). Inclination: 74.00 deg. Period: 113.60 min. COSPAR: 1972-087F. USAF Sat Cat: 6268. References: 2, 6.
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Cosmos 534 Nation: USSR. Program: Strela. Payload: Strela-1M no. 39. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,349 km (838 mi). Apogee: 1,468 km (912 mi). Inclination: 74.00 deg. Period: 114.00 min. COSPAR: 1972-087G. USAF Sat Cat: 6269. References: 2, 6.
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Cosmos 535 Nation: USSR. Program: Strela. Payload: Strela-1M no. 40. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,384 km (859 mi). Apogee: 1,468 km (912 mi). Inclination: 74.00 deg. Period: 114.40 min. COSPAR: 1972-087H. USAF Sat Cat: 6270. References: 2, 6.
1972 November 1 - 02:40 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 160 km (90 mi). References: 2.
1972 November 1 - 05:03 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.439UI. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 195 km (121 mi). References: 2.
1972 November 1 - 05:45 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NRL NB4.257. -
NRL NB4.257 Astronomy mission Nation: USA. Agency: NRL. Apogee: 200 km (120 mi). References: 2.
1972 November 1 - 09:33 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.216-2. -
HIBAL Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 220 km (130 mi). References: 2.
1972 November 2 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
FOT-3 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1972 November 2 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
FOT-3 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1972 November 2 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
FOT-3 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1972 November 2 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
FOT-3 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1972 November 2 - 04:27 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5C. LV Configuration: Black Brant VC NASA 21.02UI. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 237 km (147 mi). References: 2.
1972 November 2 - 06:10 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 6 AC. LV Configuration: Skylark 6 AC S95. -
ESRO S95 X-ray Astronomy mission Nation: UK. Agency: BAC/ESRO. Apogee: 270 km (160 mi). References: 2.
1972 November 2 - 23:28 GMT - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Canopus. Model: Rigel. -
MPE Barium release? EXP 63 Aeronomy / ionosphere mission Nation: Argentina. Agency: IIAE. Apogee: 240 km (140 mi). References: 2.
1972 November 3 - Launch Site: Baikonur. Launch Complex: LC173. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100. -
BI-4 Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1972 November 3 - 01:34 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: LC132/1?. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M Yu47121-1U. -
Cosmos 536 Nation: USSR. Program: Tselina. Mass: 875 kg (1,929 lb). Class: Sigint. Spacecraft: Tselina-O. Agency: MO SSSR. Perigee: 522 km (324 mi). Apogee: 539 km (334 mi). Inclination: 74.00 deg. Period: 95.20 min. COSPAR: 1972-088A. USAF Sat Cat: 6272. Decay Date: 1980-07-20. Possible navigation satellite. References: 2, 6.
1972 November 3 - 11:45 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P129A. -
Polar chorus Aurora mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1972 November 4 - 02:15 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.487UA. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 123 km (76 mi). References: 2.
1972 November 4 - 23:27 GMT - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Canopus. Model: Rigel. -
MPE Barium release? EXP 64 Aeronomy / ionosphere mission Nation: Argentina. Agency: IIAE. Apogee: 252 km (156 mi). References: 2.
1972 November 6 - 00:04 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk CRL A08.215-2. -
Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 212 km (131 mi). References: 2.
1972 November 8 - 08:30 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.86GG. -
Astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1972 November 8 - 22:56 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P41A. -
Particles / substorm Aurora mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1972 November 9 - -
M2 Flight 38 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 22. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Powell. Maximum Speed - 961 kph. Maximum Altitude - 14260 m. Flight Time - 364 sec. References: 49, 97.
1972 November 9 - 03:23 GMT - Launch Site: Vandenberg. Launch Complex: SLC10W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Burner 2A. LV Configuration: Thor Burner 2A 294. -
DMSP-Block-5B F3 Nation: USA. Program: DMSP. Payload: DMSP 6530. Mass: 195 kg (429 lb). Class: Earth. Type: Weather. Spacecraft: DMSP Block 5B. Agency: USAF. Perigee: 785 km (487 mi). Apogee: 841 km (522 mi). Inclination: 98.60 deg. Period: 101.10 min. COSPAR: 1972-089A. USAF Sat Cat: 6275. Defense Meteorological Satellite Program. References: 2, 6.
1972 November 10 - 01:14 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 1914. LV Configuration: Delta 1914 580/D92. -
Anik A1 Nation: Canada. Program: Anik. Payload: Telesat 1. Mass: 557 kg (1,227 lb). Class: Communications. Spacecraft: HS 333. Agency: Telesat. Perigee: 36,145 km (22,459 mi). Apogee: 36,247 km (22,522 mi). Inclination: 11.30 deg. Period: 1,457.10 min. COSPAR: 1972-090A. USAF Sat Cat: 6278. Completed Operations Date: 1982-07-15. Anik I and Anik II also registered as United States objects. .The satellites, act as space repeaters capable of receiving transmissions from earth stations and retransmitting them to other earth stations in Canada. The antenna coverage of the satellite pr ovides the capability of serving virtually all of Canada. Anik I and II had weights of 1240.59 lb and 1246.48 lb. Each satellite has 12 RF channels each capable of transmitting a color television signal or up to 900 one-way voice channels. Positioned in geosynchronous orbit over the Americas at 114 deg W in 1973-1976; over the Americas at 104 deg W in 1976-1982 As of 1 September 2001 located at 66.14 deg W drifting at 5.205 deg W per day. As of 2007 Mar 9 located at 107.03W drifting at 5.211W degrees per day.
References: 2, 6.
1972 November 11 - 08:26 GMT - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Canopus. Model: Rigel. -
MPE Barium release? EXP 65 Ionosphere mission Nation: Argentina. Agency: IIAE. Apogee: 260 km (160 mi). References: 2.
1972 November 14 - 18:48 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.02GS. -
Solar mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1972 November 15 - 22:13 GMT - Launch Site: San Marco. Launch Complex: -. Launch Pad: -. Launch Vehicle: Scout. Model: Scout D-1. LV Configuration: Scout D-1-F S170CR. -
Explorer 48 Nation: USA. Program: Explorer. Payload: SAS B. Mass: 185 kg (407 lb). Class: Solar. Spacecraft: SAS. Agency: NASA GSF. Perigee: 526 km (326 mi). Apogee: 526 km (326 mi). Inclination: 1.00 deg. Period: 95.20 min. COSPAR: 1972-091A. USAF Sat Cat: 6282. Decay Date: 1976-08-20. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1972 November 16 - Launch Vehicle: N1.
1972 November 19 - -
India-Soviet space cooperation. Nation: USSR. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On Co-operation of USSR and India on Space Research --USSR-India co-operation' was issued. References: 474.
1972 November 20 - 04:54 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 S94. -
ESRO S94 X-ray Astronomy mission Nation: Europe. Agency: ESRO. Apogee: 210 km (130 mi). References: 2.
1972 November 20 - 17:07 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.13GT. -
Test mission Nation: USA. Agency: NASA. Apogee: 250 km (150 mi). References: 2.
1972 November 21 - -
M2 Flight 39 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 23. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Manke. Maximum Speed - 1524 kph. Maximum Altitude - 20330 m. Flight Time - 377 sec. References: 49, 97.
1972 November 21 - Launch Vehicle: N1. -
State Commission was held to formally approve launch of N1 7L. Nation: USSR. Program: Lunar L3. Spacecraft: Soyuz 7K-LOK. References: 367.
1972 November 22 - 00:17 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout D-1. LV Configuration: Scout D-1-F S185C. -
ESRO 4 Nation: Europe. Mass: 114 kg (251 lb). Class: Technology. Spacecraft: ESRO. Agency: ESRO. Perigee: 245 km (152 mi). Apogee: 1,173 km (728 mi). Inclination: 91.10 deg. Period: 99.00 min. COSPAR: 1972-092A. USAF Sat Cat: 6285. Decay Date: 1974-04-15. Polar ionosphere investigations. Seventh ESRO satellite. Mass 115 kg. Also registered by the United States as 1972-92A, in A/AC.105/INF.267, with orbital parameters 98.8 min, 244 x 1160 km x 91.1 deg, category B. References: 2, 6.
1972 November 23 - Launch Vehicle: N1. -
Final N1 preparations Nation: USSR. Program: Lunar L3. Spacecraft: Soyuz 7K-LOK. At 17:00 fuelling of N1 7L began. Lox fuelling was completed at 23:40. References: 367.
1972 November 23 - 03:00 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 180 km (110 mi). References: 2.
1972 November 23 - 06:11 GMT - Launch Site: Baikonur. Launch Complex: LC110L. Launch Pad: -. Launch Vehicle: N1. Model: N1. LV Configuration: N-1 11A52 7L. FAILURE: Failure. -
N1 7L Nation: USSR. Program: Lunar L3. Payload: Soyuz 7K-LOK / LK Mockups. Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-LOK. Agency: RVSN. Apogee: 40 km (24 mi). COSPAR: F721123A. Decay Date: 1972-11-23. Unmanned test of manned lunar mission launch vehicle serial number 7L. This article incorporated significant changes to the previous model, including roll 'steering' engines to prevent the loss of control that destroyed 6L. The rocket ascended into the sky, and the engines ran 106.93 seconds, only seven seconds before completion of first stage burnout. Programmed shutdown of some engines to prevent overstressing of the structure led to propellant line hammering, rupture of propellant lines, and an explosion of engine number 4. The vehicle disintegrated.
Additional Details: N1 7L. References: 367.
1972 November 25 - Launch Site: White Sea Launch Area. Launch Complex: -. Launch Pad: 65.5 N x 38.0 E. Launch Vehicle: R-29. Model: Vysota. -
Test mission Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E. References: 2.
1972 November 25 - 02:00 GMT - Launch Site: Vandenberg. Launch Complex: LF22. Launch Pad: -. Launch Vehicle: Minuteman 3. -
OT GT18GB operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1972 November 25 - 09:10 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 537 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 203 km (126 mi). Apogee: 303 km (188 mi). Inclination: 64.00 deg. Period: 89.60 min. COSPAR: 1972-093A. USAF Sat Cat: 6287. Duration: 12.00 days. Decay Date: 1972-12-07. Area survey photo reconnaissance satellite; returned film capsule. References: 2, 6.
1972 November 28 - Launch Site: White Sea Launch Area. Launch Complex: -. Launch Pad: 65.5 N x 38.0 E. Launch Vehicle: R-29. Model: Vysota. -
Test mission Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E. References: 2.
1972 November 28 - Launch Site: White Sea Launch Area. Launch Complex: -. Launch Pad: 65.5 N x 38.0 E. Launch Vehicle: R-29. Model: Vysota. -
Test mission Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E. References: 2.
1972 November 28 - Launch Site: San Marco. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. -
Ionosphere / aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1972 November 29 - -
M2 Flight 40 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 24. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Powell. Maximum Speed - 1432 kph. Maximum Altitude - 20570 m. Flight Time - 357 sec. References: 49, 97.
1972 November 30 - 21:49 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Intercosmos 8 Nation: USSR. Program: DS. Payload: DS-U1-IK s/n 2. Mass: 340 kg (740 lb). Class: Earth. Type: Ionosphere. Spacecraft: DS-U1-IK. Agency: IK. Perigee: 203 km (126 mi). Apogee: 645 km (400 mi). Inclination: 71.00 deg. Period: 93.10 min. COSPAR: 1972-094A. USAF Sat Cat: 6291. Completed Operations Date: 1973-02-01. Decay Date: 1973-03-02. Continued joint investigation of the characteristics of the earth's ionosphere and recording of electron and proton fluxes. References: 2, 6, 99, 116.
1972 December 1 - 01:23 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3B. LV Configuration: Black Brant IIIB AND-3B-63. -
Microwave background Submillimeter radio astronomy mission Nation: Canada. Agency: NRCC. Apogee: 185 km (114 mi). References: 2.
1972 December 1 - 05:04 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 165 km (102 mi). References: 2.
1972 December 1 - 09:02 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 180 km (110 mi). References: 2.
1972 December 1 - 12:39 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 160 km (90 mi). References: 2.
1972 December 2 - 04:39 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Molniya 8K78M. -
Molniya 1-22 Nation: USSR. Program: Molniya. Payload: Molniya-1. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-1. Agency: MOM. Perigee: 462 km (287 mi). Apogee: 39,608 km (24,611 mi). Inclination: 64.00 deg. Period: 712.00 min. COSPAR: 1972-095A. USAF Sat Cat: 6294. Decay Date: 1976-02-11. Uncertain if Molniya-1T model was Molniya-1 or Molniya-1T. Operation of a system of long range telephone-telegraph radiocommunication, and transmission of USSR Central Television programmes to the stations of the Orbita network. References: 2, 6.
1972 December 5 - 02:35 GMT - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 3. -
FOT GT41GM Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1972 December 5 - 04:20 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 CRL A04.004-9. -
HISTAR 7 Infrared astronomy mission Nation: USA. Agency: AFCRL. Apogee: 179 km (111 mi). References: 2.
1972 December 5 - 07:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5C. LV Configuration: Black Brant VC CRL A18.006-5. -
Auroral infrared Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 194 km (120 mi). References: 2.
1972 December 5 - 17:30 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.509UI. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 185 km (114 mi). References: 2.
1972 December 6 - -
M2 Flight 41 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 25. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Powell. Maximum Speed - 1265 kph. Maximum Altitude - 20820 m. Flight Time - 332 sec. References: 49, 97.
1972 December 7 - 05:03 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL1202. -
GX5-1 Lunar Occultation X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 248 km (154 mi). References: 2.
1972 December 7 - 05:33 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Saturn V. Model: Saturn V. LV Configuration: Saturn V SA-512. -
Apollo 17 Nation: USA. Program: Apollo. Payload: Apollo CSM 114/LM 12/ ALSEP/ LRV-3/S-IVB-512. Mass: 30,342 kg (66,892 lb). Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo CSM. Location of Spacecraft: Space Center Houston (NASA Johnson Space Center's Visitor Center), Houston, TX. Agency: NASA MSC. Perigee: 167 km (103 mi). Apogee: 167 km (103 mi). Inclination: 28.53 deg. Period: 87.83 min. COSPAR: 1972-096A. USAF Sat Cat: 6300. Duration: 12.58 days. Decay Date: 1972-12-19. Crew: Cernan, Evans, Schmitt. Flight: Apollo 17. Apollo 17 (AS-512), the final Apollo manned lunar landing mission, was launched from Pad A, Launch Complex 39, KSC, at 12:33 a.m. EST December 7. Crew members were astronauts Eugene A. Cernan, Ronald E. Evans, and Harrison H. Schmitt. The launch had been delayed 2 hours 40 minutes by a countdown sequencer failure, the only such delay in the Apollo program caused by a hardware failure. All launch vehicle systems performed normally in achieving an earth parking orbit of 170 by 168 kilometers. After checkout, insertion into a lunar trajectory was begun at 3:46 a.m.; translunar coast time was shortened to compensate for the launch delay. CSM 114 transposition, docking with LM-12, and LM ejection from the launch vehicle stage were normal. The S-IVB stage was maneuvered for lunar impact, striking the surface about 13.5 kilometers from the preplanned point at 3:27 p.m. EST December 10. The impact was recorded by the passive seismometers left on the moon by Apollo 12, 14, 15, and 16. The crew performed a heat flow and convection demonstration and an Apollo light-flash experiment during the translunar coast. The scientific instrument module door on the SM was jettisoned at 10:17 a.m. EST December 10. The lunar orbit insertion maneuver was begun at 2:47 p.m. and the Apollo 17 spacecraft entered a lunar orbit of 315 by 97 kilometers. After separation of the LM Challenger from the CSM America and a readjustment of orbits, the LM began its powered descent and landed on the lunar surface in the Taurus-Littrow region at 2:55 p.m. EST on December 11, with Cernan and Schmitt. The first EVA began about 4 hours later (6:55 p.m.). Offloading of the lunar roving vehicle and equipment proceeded as scheduled. The Apollo Lunar Surface Experiment Package was deployed approximately 185 meters west northwest of the Challenger. Astronaut Cernan drove the lunar roving vehicle to the experiments deployment site, drilled the heat flow and deep core holes, and emplaced the neutron probe experiment. Two geological units were sampled, two explosive packages deployed, and seven traverse gravimeter measurements were taken. During the 7-hour 12-minute EVA, 14 kilograms of samples were collected. The second extravehicular activity began at 6:28 p.m. EST December 12. Because of geological interest, station stop times were modified. Orange soil was discovered and became the subject of considerable geological discussion. Five surface samples and a double core sample were taken in the area of the orange soil. Three explosive packages were deployed, seven traverse gravimeter measurements were taken, and observations were photographed. Samples collected totaled 34 kilograms during the 7 hours and 37 minutes of the second EVA. The third and final EVA began at 5:26 p.m. EST December 13. Specific sampling objectives were accomplished. Samples - including blue-gray breccias, fine-grained vesicular basalts, crushed anorthositic rocks, and soils - weighed 66 kilograms. Nine traverse gravimeter measurements were made. The surface electrical properties experiment was terminated. Before reentering the LM, the crew selected a breccia rock to dedicate to the nations represented by students visiting the Mission Control Center. A plaque on the landing gear of the lunar module, commemorating all of the Apollo lunar landings, was then unveiled. After 7 hours 15 minutes, the last Apollo EVA on the lunar surface ended. Total time of the three EVAs was approximately 22 hours; the lunar roving vehicle was driven 35 kilometers, and about 115 kilograms of lunar sample material was acquired. While Cernan and Schmitt were exploring the lunar surface, Evans was conducting numerous scientific activities in the CSM in lunar orbit. In addition to the panoramic camera, the mapping camera, and the laser altimeter, three new scientific instrument module experiments were included in the Apollo 17 orbital science equipment. An ultraviolet spectrometer measured lunar atmospheric density and composition; an infrared radiometer mapped the thermal characteristics of the moon; and a lunar sounder acquired data on the subsurface structure. Challenger lifted off the moon at 5:55 p.m. EST December 14. Rendezvous with the orbiting CSM and docking were normal. The two astronauts transferred to the CM with samples and equipment and the LM ascent stage was jettisoned at 1:31 a.m. December 15. Its impact on the lunar surface about 1.6 kilometers from the planned target was recorded by four Apollo 17 geophones and the Apollo 12, 14, 15, and 16 seismometers emplaced on the surface. The seismic experiment explosive packages that had been deployed on the moon were detonated as planned and recorded on the geophones. During the coast back to earth, Evans left the CSM at 3:27 p.m. EST December 17 for a 1-hour 7-minute inflight EVA and retrieved lunar sounder film and panoramic and mapping camera cassettes from the scientific instrument module bay. The crew conducted the Apollo light- flash experiment and operated the infrared radiometer and ultraviolet spectrometer. Reentry, landing, and recovery were normal. The command module parachuted into the mid-Pacific at 2:25 p.m. EST December 19, 6.4 kilometers from the prime recovery ship, U.S.S. Ticonderoga. The crew was picked up by helicopter and was on board the U.S.S. Ticonderoga 52 minutes after the CM landed. All primary mission objectives had been achieved.
References: 2, 6, 16, 26, 27, 33,60.
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Apollo 17 LM Nation: USA. Program: Apollo. Payload: Apollo LM 12. Mass: 16,448 kg (36,261 lb). Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo LM. Agency: NASA MSC. Perigee: 167 km (103 mi). Apogee: 167 km (103 mi). Inclination: 28.53 deg. Period: 87.83 min. COSPAR: 1972-096x. USAF Sat Cat: 6300. Duration: 12.58 days. Decay Date: 1972-12-19. Flight: Apollo 17. References: 2, 6, 16, 26, 27, 33,60.
1972 December 7 - 05:45 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Ute Tomahawk. LV Configuration: Ute Tomahawk CRL A09.107-2. -
Auroral composition Aeronomy mission Nation: USA. Agency: USAF CRL. Apogee: 171 km (106 mi). References: 2.
1972 December 7 - 07:07 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.307-3. -
7-in Density Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 210 km (130 mi). References: 2.
1972 December 8 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. -
SSTTP M2-21 Target mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1972 December 8 - 06:26 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.83UG. -
Astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1972 December 11 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
FOT-4 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1972 December 11 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
FOT-4 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1972 December 11 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
FOT-4 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1972 December 11 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
FOT-4 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1972 December 11 - 00:00 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL1005. -
Ions / O2 Ionosphere mission Nation: UK. Agency: BAC. Apogee: 196 km (121 mi). References: 2.
1972 December 11 - 01:30 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.107-3. -
Auroral composition Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 136 km (84 mi). References: 2.
1972 December 11 - 01:39 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.301-1. -
7-in Density Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 255 km (158 mi). References: 2.
1972 December 11 - 07:56 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 0900. LV Configuration: Delta 0900 577/D93. -
Nimbus 5 Nation: USA. Payload: Nimbus E. Mass: 722 kg (1,591 lb). Class: Earth. Type: Weather. Spacecraft: Nimbus. Agency: NASA GSF. Perigee: 1,088 km (676 mi). Apogee: 1,101 km (684 mi). Inclination: 100.10 deg. Period: 107.20 min. COSPAR: 1972-097A. USAF Sat Cat: 6305. Environmental research. Primary experiments included a temperature-humidity infrared radiometer (THIR) for measuring day and night surface and cloudtop temperatures as well as the water vapor content of the upper atmosphere, electrically scanning microwave radiometer (ESMR) for mapping the microwave radiation from the earth's surface and atmosphere, infrared temperature profile radiometer (ITPR) for obtaining vertical profiles of temperature and moisture, Nimbus E microwave spectrometer (NEMS) for determining tropospheric temperature profiles, atmospheric water vapor abundances, and cloud liquid water contents, selective chopper radiometer (SCR) for observing the global temperature structure of the atmosphere, and a surface composition mapping radiometer (SCMR) for measuring the differences in the thermal emission characteristics of the earth's surface.
References: 2, 6.
1972 December 11 - 21:38 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170A. LV Configuration: Aerobee 170A NASA 13.96UA. -
JHU Airglow 12 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 214 km (132 mi). References: 2.
1972 December 12 - Launch Site: Vandenberg. Launch Complex: LF25. Launch Pad: -. Launch Vehicle: Minuteman 3. -
OT GT19GB operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1972 December 12 - Launch Site: Vandenberg. Launch Complex: LF26. Launch Pad: LF26?. Launch Vehicle: Minuteman 3. -
OT GT20GB operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1972 December 12 - 06:51 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. -
Molniya 2-04 Nation: USSR. Program: Molniya. Payload: Molniya-2. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-2. Agency: MOM. Perigee: 507 km (315 mi). Apogee: 39,284 km (24,409 mi). Inclination: 65.30 deg. Period: 706.40 min. COSPAR: 1972-098A. USAF Sat Cat: 6308. Decay Date: 1975-01-22. Continued operation of the long-range telephone and telegraph radio-communication system; transmission of USSR central television programmes to stations in the Orbita network and international cooperation. References: 2, 6.
1972 December 12 - 23:54 GMT - -
EVA Apollo 17-1 Nation: USA. Program: Apollo. Class: Manned. Type: Lunar lander. Spacecraft: Apollo LM. Crew: Cernan, Schmitt. Flight: Apollo 17. EVA Duration: 0.30 days. Explored lunar surface near LM and deployed ALSEP unmanned scientific station equipment. References: 66.
1972 December 13 - -
M2 Flight 42 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 26. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Dana. Fastest M2-F3 flight. Maximum Speed - 1712 kph. Maximum Altitude - 20330 m. Flight Time - 383 sec. References: 49, 97.
1972 December 13 - 05:18 GMT - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 1. LV Configuration: Dragon D-38. -
FU-206 Protons / electrons Ionosphere / geocorona mission Nation: France. Agency: CNES. Apogee: 380 km (230 mi). References: 2.
1972 December 13 - 14:19 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Micon. Model: Zenit. LV Configuration: Zenit-C Zenit-Cuckoo. -
DLR A-ZC-48 Astrik Ionosphere mission Nation: Germany. Agency: DFVLR. Apogee: 144 km (89 mi). References: 2.
1972 December 13 - 21:03 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.94US. -
Solar mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1972 December 13 - 21:23 GMT - Launch Site: Syowa Base. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-210. LV Configuration: S-210JA-7. -
Aurora / ionosphere / fields mission Nation: Japan. Agency: NIPR. Apogee: 126 km (78 mi). References: 2.
1972 December 13 - 23:28 GMT -
1972 December 14 - Launch Site: White Sea Launch Area. Launch Complex: -. Launch Pad: 65.5 N x 38.0 E. Launch Vehicle: R-29. Model: Vysota. -
Test mission Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E. References: 2.
1972 December 14 - Launch Site: White Sea Launch Area. Launch Complex: -. Launch Pad: 65.5 N x 38.0 E. Launch Vehicle: R-29. Model: Vysota. -
Test mission Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E. References: 2.
1972 December 14 - Launch Site: White Sea Launch Area. Launch Complex: -. Launch Pad: 65.5 N x 38.0 E. Launch Vehicle: R-29. Model: Vysota. -
Test mission Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E. References: 2.
1972 December 14 - Launch Site: White Sea Launch Area. Launch Complex: -. Launch Pad: 65.5 N x 38.0 E. Launch Vehicle: R-29. Model: Vysota. -
Test mission Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E. References: 2.
1972 December 14 - 13:40 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 538 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 205 km (127 mi). Apogee: 283 km (175 mi). Inclination: 65.40 deg. Period: 89.40 min. COSPAR: 1972-099A. USAF Sat Cat: 6311. Duration: 13.00 days. Decay Date: 1972-12-27. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1972 December 14 - 22:25 GMT -
1972 December 15 - -
EVA Apollo 17-5 Nation: USA. Program: Apollo. Class: Manned. Type: Lunar lander. Spacecraft: Apollo LM. Crew: Cernan, Schmitt. Flight: Apollo 17. EVA Duration: 0.0007 days. Threw excess equipment out of LM before lift-off. References: 66.
1972 December 15 - -
EVA Apollo 17-4 Nation: USA. Program: Apollo. Class: Manned. Type: Lunar lander. Spacecraft: Apollo LM. Crew: Cernan, Schmitt. Flight: Apollo 17. EVA Duration: 0.0014 days. Threw excess equipment out of LM before lift-off. References: 66.
1972 December 15 - 21:25 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1972 December 16 - -
Elektro, Meteor-3 weather satellites authorised Nation: USSR. Spacecraft: Elektro, Meteor-3. Military-Industrial Commission (VPK) Decree 'On establishment of the Planeta-S weather satellite system' was issued. The resolution ordered development of a third generation system. This used the Planeta-S sensor package in the non-co-orbital Meteor-3 system plus the geostationary system Elektro, which was to begin tests in 1982. Elektro suffered numerous delays due to equipment and software problems. Flight trials of Meteor-3 did not begin until 1984, and there was only a single launch of Elektro, in 1994.
1972 December 16 - 11:24 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout D-1. LV Configuration: Scout D-1-F S181C. -
Aeros 1 Nation: Germany. Payload: GRS B. Mass: 127 kg (279 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Aeros. Agency: DFVLR. Perigee: 223 km (138 mi). Apogee: 867 km (538 mi). Inclination: 96.90 deg. Period: 95.60 min. COSPAR: 1972-100A. USAF Sat Cat: 6315. Decay Date: 1973-08-22. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1972 December 17 - 20:27 GMT - -
EVA Apollo 17-6 Nation: USA. Program: Apollo. Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo CSM. Crew: Evans, Schmitt . Flight: Apollo 17. EVA Duration: 0.0458 days. Deep space retrieval of film cartridges from Service Module. References: 66.
1972 December 18 - 21:15 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1972 December 19 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. -
HK-3 Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1972 December 19 - -
Landing of Apollo 17 Nation: USA. Program: Apollo. Flight: Apollo 17. Reentry, landing, and recovery were normal. The Apollo 17 command module parachuted into the mid-Pacific at 19:25 GMT, 6.4 kilometers from the prime recovery ship, U.S.S. Ticonderoga. The crew was picked up by helicopter and was on board the U.S.S. Ticonderoga 52 minutes after the CM landed. Manned exploration of the moon had ended.
1972 December 20 - 22:20 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3A Agena D. LV Configuration: SLV-3A Agena D 5204A / Agena D A 2805. -
Canyon 5 Nation: USA. Payload: Canyon Improved. Mass: 700 kg (1,540 lb). Class: Sigint. Spacecraft: Canyon. Agency: NRO/USAF. Perigee: 31,012 km (19,269 mi). Apogee: 40,728 km (25,307 mi). Inclination: 9.70 deg. Period: 1,440.40 min. COSPAR: 1972-101A. USAF Sat Cat: 6317. First launch of improved ELINT satellite. In comparison to earlier Canyon ELINT satellites, Improved Canyon had a similar but heavier payload which separated from the Agena D final stage. References: 2, 6, 172, 278.
1972 December 21 - -
M2 Flight 43 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 27. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Manke. Last M2-F3 flight, also highest. Maximum Speed - 1377 kph. Maximum Altitude - 21790 m. Flight Time - 390 sec. References: 49, 97.
1972 December 21 - -
Zenit-4MKT authorised Nation: USSR. Spacecraft: Zenit-4MKT. Decree of 21 December 1972 started work on this replacement to the Meteor-Priroda system. The spacecraft was an adaptation of the recoverable Zenit/Vostok spacecraft for remote sensing.
1972 December 21 - 02:05 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M Yu149-43. -
Cosmos 539 Nation: USSR. Mass: 600 kg (1,320 lb). Spacecraft: Sfera. Agency: MO SSSR. Perigee: 1,342 km (833 mi). Apogee: 1,379 km (856 mi). Inclination: 74.00 deg. Period: 112.90 min. COSPAR: 1972-102A. USAF Sat Cat: 6319. Investigation of the upper atmosphere and outer space. References: 2, 6.
1972 December 21 - 17:45 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 24B. LV Configuration: Titan 24B 24B-6 (3B-40). -
OPS 3978 Nation: USA. Payload: KH-8 no. 37 / 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: 378 km (234 mi). Inclination: 110.50 deg. Period: 89.70 min. COSPAR: 1972-103A. USAF Sat Cat: 6321. Decay Date: 1973-01-23. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1972 December 22 - 04:55 GMT - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 2. -
FOT GT111M Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1972 December 22 - 05:00 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission? Nation: USSR. Agency: AN SSSR. Apogee: 160 km (90 mi). References: 2.
1972 December 25 - 23:05 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53724-113. -
Cosmos 540 Nation: USSR. Program: Strela. Mass: 750 kg (1,650 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-2M. Agency: MO SSSR. Perigee: 763 km (474 mi). Apogee: 790 km (490 mi). Inclination: 74.10 deg. Period: 100.40 min. COSPAR: 1972-104A. USAF Sat Cat: 6323. References: 2, 6.
1972 December 26 - Launch Site: Baikonur. Launch Complex: LC173. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100. -
BI-4 Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1972 December 27 - 10:30 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511M. -
Cosmos 541 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MT. Agency: MOM. Perigee: 218 km (135 mi). Apogee: 348 km (216 mi). Inclination: 81.00 deg. Period: 90.20 min. COSPAR: 1972-105A. USAF Sat Cat: 6326. Duration: 12.00 days. Decay Date: 1973-01-08. Military topography satellite; returned film capsule; separated science capsule. References: 2, 6.
1972 December 28 - 11:00 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launc |