1969 October 1 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. -
Eniwetok Atoll placed on a caretaker status Nation: USA. References: 88.
1969 October 1 - -
Problems with Beregovoi. Nation: USSR. Program: Soyuz. Kamanin notes that Beregovoi is not doing well as chief of the cosmonaut centre. But he still feels no other cosmonaut has any better leadership qualities. References: 376.
1969 October 1 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 HRV. Launch Vehicle: Stonechat. Model: Stonechat I. LV Configuration: Stonechat I F.00. -
HRV 933 test Nation: UK. Agency: RAE. Apogee: 30 km (18 mi). References: 2.
1969 October 1 - Launch Site: Vandenberg. Launch Complex: LF21. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2510. -
ST Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1969 October 1 - 01:20 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P52H. -
Night D / E-region Ionosphere mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1969 October 1 - 04:19 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P51H. -
Night D / E-region Ionosphere mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1969 October 1 - 22:29 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout B. LV Configuration: Scout B S172C. FAILURE: Partial Failure. -
ESRO 1B Nation: Europe. Payload: Boreas. Mass: 80 kg (176 lb). Class: Technology. Spacecraft: ESRO. Agency: ESRO. Perigee: 298 km (185 mi). Apogee: 378 km (234 mi). Inclination: 85.00 deg. Period: 91.30 min. COSPAR: 1969-083A. USAF Sat Cat: 4114. Decay Date: 1969-11-23. Ionospheric and auroral investigations; lower than planned orbit. Fourth satellite of ESRO. Also registered by the United States in A/AC.105/INF.220 as United States space object 1969-83A, with category B and orbital parameters 90.6 min, 280 x 339 km x 85.1 deg.
References: 2, 6.
1969 October 2 - -
Soyuz 6/7/8 State Commission Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. The State Commission convenes at Tyuratam and affirms everything is ready for the Soyuz 6/7/8 flight. References: 376.
1969 October 3 - -
Mishin arrives at Tyuratam. Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Kamanin notes he now always shows up only after the State Commission has met. References: 376.
1969 October 3 - 01:00 GMT - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1173. -
FOT GT44B Follow-on Test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1969 October 3 - 02:24 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150 MI. LV Configuration: Aerobee 150 MI-20 NASA 04.279UG. -
Astronomy mission Nation: USA. Agency: NASA. Apogee: 158 km (98 mi). References: 2.
1969 October 4 - 05:15 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.71UG. -
CRL AH08.645 X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1969 October 5 - -
DOS Conspiracy briefed to Ustinov Nation: USSR. Program: Lunar L3, Almaz, Salyut. Spacecraft: LK, Soyuz 7K-LOK. Mishin was opposed to the DOS space station concept - he wanted to pursue the N1-launched MKBS. Afanasyev and Deputy Minister Tyulin wouldn't support the idea either. None of them wanted to take the risk. The only chance was to get to VPK Chairman Ustinov through Communist party channels. The opportunity came on the flight of engineers and management to Baikonur for the Soyuz 6/7/8 flight. Feoktistov had prepared a briefing on DOS, which he presented to Ustinov.
References: 367.
1969 October 5 - -
Sunday at the cosmodrome Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. It is agreed that future pre-flight reviews of spacecraft operations should not just be limited to standard procedures, but should cover back-up and emergency procedures as well, even though this will take 2 to 3 days longer to prepare. It is Sunday at the cosmodrome. Kamanin gives a speech on the Gagarin launch in 1961. There are chess, tennis, billiards, and ping-pong tournaments.
References: 376.
1969 October 5 - 22:28 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S29/1. -
ESRO S29 / 1 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 225 km (139 mi). References: 2.
1969 October 6 - -
Soyuz 6/7/8 experiment review Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Meeting between the Soyuz 6/7/8 crews and engineers. Shatalov pushes his idea for a manually flown spacecraft rendezvous, provided that Soyuz 7 and 8 visually acquire each other immediately after Soyuz 8 is put into orbit. He believes this would not only save time and fuel, but also provide the chance to develop procedures for interception of non-cooperative enemy satellites. Mishin rejects the idea, seeing a doubling of risk of an unsuccessful flight. The fact is, the Soyuz is only equipped for automatic docking. There are no on-board indicators of range and range-rate to target - necessary inputs for any manual docking. The view through the periscope is the only forward-looking view available to the crew, and it is inadequate for manual docking.
Additional Details: Soyuz 6/7/8 experiment review. References: 376.
1969 October 6 - Launch Site: White Sands. Launch Complex: LC50. Launch Pad: -. Launch Vehicle: Sprint. LV Configuration: Sprint ABM FLA-36. FAILURE: Failure. -
Test mission Nation: USA. Agency: USA. Apogee: 0 km ( mi). References: 2.
1969 October 6 - 01:45 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M. -
Meteor 1-02 Nation: USSR. Payload: Meteor M no. 2. Mass: 3,800 kg (8,300 lb). Class: Earth. Type: Weather. Spacecraft: Meteor M. Agency: MOM. Perigee: 513 km (318 mi). Apogee: 552 km (342 mi). Inclination: 81.20 deg. Period: 95.30 min. COSPAR: 1969-084A. USAF Sat Cat: 4119. Decay Date: 2002-08-20. Cloud and ice cover imaging; investigated IR, thermal reflection/radiation from Earth's atmosphere. Acquisition of meteorological information needed for use by the weather service. References: 2, 6.
1969 October 8 - -
Soyuz 6/7/8 State Commission Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Kamanin takes General Efimov to see the roll-out of the Soyuz 6 booster. Mishin calls during the tour to ask that Volkov be switched with TsKBEM engineer Grechko on the Soyuz 7 crew. Kamanin refuses at this late date, noting in disgust Mishin is always pushing his staff for flight regardless of how it might affect the mission. Efimov is then taken to see the N1 MIK assembly building, the largest building in Europe. They view the construction of the 104-m-long booster's three stages. Next they go out to the pad, surveying the facility from 120 m up in one of the gantries. Kamanin muses that unless the N1 can be made reliable, the Russians will be 7 to 8 years behind the Americans in planetary and lunar exploration. Later the State Commission meets and fixes the launch schedule for the upcoming flights. Mishin does not raise the issue of Grechko flying to the commission. Shatalov is named commander of the entire three-spacecraft group flight.
References: 376.
1969 October 9 - -
Final preparations Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. The ship's logs/flight plans are reviewed one more time. Tyuratam commander General Kurushin runs through the Svinets ABM experiment again with Shonin and Kubasov - they're ready. The Communist Party has selected Beregovoi and Feoktistov for the trip to the United States in November, ignoring Kamanin's recommendation of Belyayev and Shatalov. Kamanin is not so much against Beregovoi, but he firmly believes that Feoktistov is not worthy of the privilege - he's a degenerate, now on this third marriage..
References: 376.
1969 October 10 - -
Major milestones for the Apollo 16-20 missions Nation: USA. Program: Apollo. Spacecraft: A7L. Flight: Apollo 16. Major milestones were reached for extending astronauts' staytime on the moon and increasing their mobility for the Apollo 16-20 missions. Modifications in the A7L spacesuit incorporating improved waist mobility were authorized, and letter contract authority for the portable life support system secondary life support system was approved.
References: 16.
1969 October 10 - -
Cosmonaut awards discussed. Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Bad weather at the cosmodrome - rain and 12-15 m/s wind. The traditional meeting of the cosmonauts and their support teams takes place at 15:00 at Area 31. Afterwards Kamanin meets with VVS General I M Moroz and Efimov. The future policy is that a cosmonaut will receive the Hero of the Soviet Union award and a military promotion only on their first flight into space. On later flights they will receive a lesser decoration and a cash award. Exceptions would be made for exceptional missions. Mozzhorin disagrees, preferring to keep things as they are.
References: 376.
1969 October 10 - Launch Site: Vandenberg. Launch Complex: 576A3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F/Trident. LV Configuration: Atlas F/Trident 98F. FAILURE: Failure. -
RMP-B-13 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 10 km (6 mi). References: 2.
1969 October 10 - 01:19 GMT - Launch Site: Resolute Bay. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Boosted Arcas 2. LV Configuration: Boosted Arcas 2 NASA 15.53GI. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 110 km (60 mi). References: 2.
1969 October 10 - 06:50 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P20H. -
SpE Ionosphere mission Nation: UK. Agency: SRC. Apogee: 130 km (80 mi). References: 2.
1969 October 10 - 20:01 GMT - Launch Site: Kiruna. Launch Complex: C. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C52/2. -
ESRO C52 / 2 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 135 km (83 mi). References: 2.
1969 October 11 - 02:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AH07.890. -
AH7.893 in FC Aeronomy mission Nation: USA. Agency: USAF. Apogee: 118 km (73 mi). References: 2.
1969 October 11 - 11:05 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 45.0 N x 46.0 W. Launch Vehicle: MR-12. -
Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 158 km (98 mi). References: 2.
1969 October 11 - 11:10 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511. -
Soyuz 6 Nation: USSR. Program: Soyuz. Payload: Soyuz 7K-OK s/n 14. Mass: 6,577 kg (14,499 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-OK. Agency: MOM. Perigee: 212 km (131 mi). Apogee: 218 km (135 mi). Inclination: 51.60 deg. Period: 88.80 min. COSPAR: 1969-085A. USAF Sat Cat: 4122. Duration: 4.95 days. Decay Date: 1969-10-16. Crew: Kubasov, Shonin. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Tested spacecraft systems and designs, manoeuvring of space craft with respect to each other in orbit, conducted scientific, technical and medico-biological experiments in group flight. Carried Vulkan welding furnace for vacuum welding experiments in depressurized orbital module. Was to have taken spectacular motion pictures of Soyuz 7 - Soyuz 8 docking but failure of rendezvous electronics in all three craft due to new helium pressurization integrity test prior to mission did not permit successful rendezvous and dockings.
Additional Details: Soyuz 6. References: 2, 6, 32, 33, 60, 376.
1969 October 11 - 19:36 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P38H. -
E fields Ionosphere mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1969 October 12 -
1969 October 12 - 10:44 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511. -
Soyuz 7 Nation: USSR. Program: Soyuz. Payload: Soyuz 7K-OK s/n 15. Mass: 6,570 kg (14,480 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-OK. Agency: MOM. Perigee: 210 km (130 mi). Apogee: 223 km (138 mi). Inclination: 51.70 deg. Period: 88.80 min. COSPAR: 1969-086A. USAF Sat Cat: 4124. Duration: 4.94 days. Decay Date: 1969-10-17. Crew: Filipchenko, Gorbatko, Volkov. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Tested spacecraft systems and designs, manoeuvring of space craft with respect to each other in orbit, conducted scientific, technical and medico-biological experiments in group flight. Was to have docked with Soyuz 8 and transferred crew while Soyuz 6 took film from nearby. However failure of rendezvous electronics in all three craft due to a new helium pressurization integrity test prior to the mission did not permit successful rendezvous and dockings.
Additional Details: Soyuz 7. References: 2, 6, 32, 33, 60, 376.
1969 October 13 - Launch Site: Vandenberg. Launch Complex: LF24. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2054. -
OT GT22F operational test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1969 October 13 - Launch Site: Biscarosse. Launch Complex: BLB. Launch Pad: -. Launch Vehicle: SSBS. Model: SSBS S02. LV Configuration: SSBS S02 C2. -
S02C-2 test Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi). References: 2.
1969 October 13 - 10:19 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511. -
Soyuz 8 Nation: USSR. Program: Soyuz. Payload: Soyuz 7K-OK s/n 16. Mass: 6,646 kg (14,651 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-OK. Agency: MOM. Perigee: 201 km (124 mi). Apogee: 227 km (141 mi). Inclination: 51.70 deg. Period: 88.70 min. COSPAR: 1969-087A. USAF Sat Cat: 4126. Duration: 4.95 days. Decay Date: 1969-10-18. Crew: Shatalov, Yeliseyev. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Tested spacecraft systems and designs, manoeuvring of space craft with respect to each other in orbit, conducted scientific, technical and medico-biological experiments in group flight. Was to have docked with Soyuz 7 and transferred crew while Soyuz 6 took film from nearby. However failure of rendezvous electronics in all three craft due to a new helium pressurization integrity test prior to the mission did not permit successful rendezvous and dockings. Recovered October 18, 1969 10:19 GMT.
Additional Details: Soyuz 8. References: 2, 6, 32, 33, 60, 376.
1969 October 14 - -
Soyuz 7-8 docking problem Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Orbital manoeuvres for the Soyuz 7-8 docking have proceeded normally. The automated rendezvous system is supposed to kick in when the spacecraft are 250 km apart. The plan is that Soyuz 7 and 8 will dock while Soyuz 6 observes from only 50 m away. However when Soyuz 7 and 8 are only a kilometre apart, the Igla automated docking system fails. The crews could conduct a manual rendezvous, but the this is not allowed by the technical flight controller.
Additional Details: Soyuz 7-8 docking problem. References: 376.
1969 October 14 - 04:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NRL NC3.136. -
Aeronomy mission Nation: USA. Agency: NRL. Apogee: 217 km (134 mi). References: 2.
1969 October 14 - 08:22 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.
1969 October 14 - 13:19 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/4. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. LV Configuration: Kosmos 11K63 2I. -
Intercosmos 1 Nation: USSR. Program: DS. Payload: DS-U3-IK s/n 1. Mass: 320 kg (700 lb). Class: Earth. Type: Magnetosphere. Spacecraft: DS-U3-IK. Agency: IK. Perigee: 264 km (164 mi). Apogee: 617 km (383 mi). Inclination: 48.30 deg. Period: 93.40 min. COSPAR: 1969-088A. USAF Sat Cat: 4128. Completed Operations Date: 1969-10-30. Decay Date: 1970-01-02. Measurements of the solar radiation and its effect on the atmosphere of the earth. Payload included East European experiments to study solar ultraviolet and X-ray effects on the upper atmosphere. Investigation of References: 2, 6, 99, 116.
1969 October 14 - 18:43 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P14H. -
D / E regions Ionosphere mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1969 October 15 - -
Second attempt to dock Soyuz 7 & 8 - rendezvous of Soyuz 6 with Soyuz 8 Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Following an orbital correction during the night, Soyuz 7 and 8 are expected to be less than 1 km from each other when communications are regained at 9 am. Instead they are 40 km apart. It will require two more orbits over Soviet territory to refine the tracking of the spacecraft and recalculate the necessary rendezvous manoeuvres. By 12:40 they are 1700 m apart and the crews begin the manual rendezvous manoeuvre. Shatalov fires his engines four times, but in the absence of any indication to the pilot of range to the target, he could not get into a position for a safe docking. He withdraws to a safe distance.
Additional Details: Second attempt to dock Soyuz 7 & 8 - rendezvous of Soyuz 6 with Soyuz 8. References: 376.
1969 October 15 - 11:16 GMT - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-305. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1969 October 15 - 15:30 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3E. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 15 - 18:46 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 SL861. -
Grenades / TMA release / Barium release Aeronomy /ionosphere mission Nation: UK. Agency: BAC. Apogee: 318 km (197 mi). References: 2.
1969 October 15 - 19:10 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3E. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 15 - 22:43 GMT - Launch Site: Wallops Island. Launch Complex: LA2. Launch Pad: LA2A?. Launch Vehicle: Astrobee. Model: Astrobee 1500. LV Configuration: Astrobee 1500 NASA 16.06GR. -
RAE-B Test Radio astronomy mission Nation: USA. Agency: NASA. Apogee: 2,575 km (1,600 mi). References: 2.
1969 October 16 - -
Landing of Soyuz 6 - further attempts to dock Soyuz 7 and 8 Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Soyuz 6 lands successfully at 09:52 GM, coming to rest in a vertical position. A recovery helicopter lands 10 minutes later, finding the cosmonauts have already emerged from the capsule. After the landing of Soyuz 6 there are two further attempts to dock Soyuz 7 and Soyuz 8, but they fail due to large errors in the ballistic calculations of the manoeuvres necessary to correct their orbits.
References: 376.
1969 October 16 - 10:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.256GG. -
Zeta Ori study Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 205 km (127 mi). References: 2.
1969 October 17 - -
Landing of Soyuz 7 Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 6, Soyuz 7, Soyuz 8. The landing commission meets at the command post at 08:00. Soyuz 7 is to land on orbit 97, beginning a 95 m/s retrofire impulse at 11:44:11. The main parachute is to deploy at 12:12:34. All is reported normal aboard the spacecraft, except that the Soyuz 7 warning light panel shows 'ASP' - automatic landing sequence. Despite this, Soyuz 7 landed successfully at 09:26 GMT.
Additional Details: Landing of Soyuz 7. References: 376.
1969 October 17 - 07:05 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P16H. -
SpE Ionosphere mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi). References: 2.
1969 October 17 - 09:15 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 SL862. -
Grenades / TMA release / Barium release Aeronomy /ionosphere mission Nation: UK. Agency: BAC. Apogee: 318 km (197 mi). References: 2.
1969 October 17 - 11:45 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 302 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: MOM. Perigee: 198 km (123 mi). Apogee: 321 km (199 mi). Inclination: 65.40 deg. Period: 89.70 min. COSPAR: 1969-089A. USAF Sat Cat: 4130. Duration: 8.00 days. Decay Date: 1969-10-25. High resolution photo reconnaissance satellite; returned film capsule References: 2, 6.
1969 October 17 - 22:09 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 166 km (103 mi). References: 2.
1969 October 17 - 22:27 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S29/2. -
ESRO S29 / 2 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 225 km (139 mi). References: 2.
1969 October 18 - -
Landing of Soyuz 8 Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Kamanin's 61st birthday begins with a communications session with Soyuz 8. Yells come from the spacecraft. What's wrong? the ground nervously inquires. They reply they are only celebrating the successful closing of the hatch, and the glowing 'SA hermetic' indication on the panel. This ends fears they had all during the flight of not being able to get the hatch closed with the broken wheel spoke. The 145 second long retrofire begins at 11:29. It looks OK on the telemetry, but Shatalov reports on UHF that the indication aboard the spacecraft was that there was a 4 second underburn. Nevertheless the landing proceeds normally, and there is a loud 'Ura!' at the command point once word of a safe crew recovery is received - the mission is completed. Soyuz 8 landed at 09:10 GMT. At 16:40 the teams head back toward Moscow aboard an Il-18. Kamanin discusses the necessity to complete an extra 8 to 10 Soyuz spacecraft. He is supported by Afanasyev and Kerimov, but Mishin and Karas are opposed now. Kamanin thinks it is insane how Soviet space progress is blocked by these kinds of politics.
References: 376.
1969 October 18 - 10:00 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 303 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 28. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 270 km (160 mi). Apogee: 466 km (289 mi). Inclination: 71.00 deg. Period: 91.90 min. COSPAR: 1969-090A. USAF Sat Cat: 4136. Completed Operations Date: 1970-01-24. Decay Date: 1970-01-23. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1969 October 18 - 11:07 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 45.0 N x 46.0 W. Launch Vehicle: MR-12. -
Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 165 km (102 mi). References: 2.
1969 October 18 - 17:47 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 45.0 N x 46.0 W. Launch Vehicle: MR-12. -
Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 160 km (90 mi). References: 2.
1969 October 19 - -
Post mortem on the Soyuz 6-7-8 mission Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 6, Soyuz 7, Soyuz 8. State commission meets to do a post mortem on the Soyuz 6-7-8 mission. Kamanin gives a 15-minute briefing on the readiness of the crews for flight. He pointed to the need for more information and training on manual flight and navigation of the spacecraft, and more active use of the pilots throughout the mission. Then the commission acts out a few scenes of their meting for the press, television, and a documentary filmmaker. The Soyuz crews are undergoing medical exams at Area 17 at Baikonur.
References: 376.
1969 October 19 - -
DOS Conspiracy briefed to wide circle of space planners Nation: USSR. Program: Lunar L3, Almaz, Salyut. Spacecraft: LK, Soyuz 7K-LOK, Almaz OPS, Salyut 1. In the euphoria after the return of the Soyuz 6/7/8 crews, the problem was how to get Ustinov to meet further with the DOS 'conspirators'. Mishin had prohibited any meetings by TsKBEM staff with the Communist Party Secretary unless Mishin was also present. Another obstacle was that Feoktistov was not a party member; how could his presence at a party meeting be explained to Mishin later? In any event these consideations were simply ignored. Feoktistov was present at a party meeting with Keldysh, Afanasyev, Tyulin, Serbin, and the Ministry of Defence's party cell: Strogonov, Kravtsev, and Popov. Keldysh was mainly worried how the project would affect the N1, but was reassured that the N1 had a dedicated work force, and the L3 lunar lander spacecraft engineers and workers that would work on DOS were currently idle and had no part of that work. It was finally decided to go ahead with the DOS no earlier than January, to allow time for Ministry Decrees, approval of a work plan by the VPK, preparation of a decree for signature by the Central Committee of the Communist Party and the Soviet Ministers. Work began on the project in December 1969 under the initial auspices of the Academy of Sciences.
Additional Details: DOS Conspiracy briefed to wide circle of space planners. References: 367.
1969 October 20 - -
Weight loss of Soyuz 6-7-8 crew Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. The medical reports show all the cosmonauts lost 1.5 to 3.5 kg during the flight (with Filipchenko having the greatest loss). However Kamanin plays tennis with Gorbatko, Shonin, and Volkov just two days after the flight. They show no apparent ill effects of zero-G.
References: 376.
1969 October 20 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 20 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 20 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 20 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 20 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 20 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 20 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 20 - 07:28 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL586. -
UK SL586 test Nation: UK. Agency: BAC. Apogee: 223 km (138 mi). References: 2.
1969 October 21 - -
Cosmonaut press conference at Baikonur Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. The cosmonauts hold a press conference on their flight. They are only allowed to speak one of ten prepared responses to questions, despite Kamanin's objections. References: 376.
1969 October 21 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1134. -
FOT GT45B Follow-on Test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1969 October 21 - 12:32 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 164 km (101 mi). References: 2.
1969 October 21 - 12:49 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: LC132/pad?. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. -
Cosmos 304 Nation: USSR. Mass: 795 kg (1,752 lb). Class: Navigation. Spacecraft: Tsiklon. Agency: MO SSSR. Perigee: 731 km (454 mi). Apogee: 748 km (464 mi). Inclination: 74.00 deg. Period: 99.60 min. COSPAR: 1969-091A. USAF Sat Cat: 4138. Military navigation satellite. References: 2, 6.
1969 October 22 - -
X-24 Flight 6 Nation: USA. Payload: X-24A flight 6. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Manke. Glide. Maximum Speed - 623 kph. Maximum Altitude - 12190 m. Flight Time - 238 sec. References: 49, 97.
1969 October 22 - -
Opposition to a major effort to develop a lunar flyer until after the Apollo 16 mission Nation: USA. Program: Apollo. Spacecraft: LFV North American. Flight: Apollo 11, Apollo 16. The Flight Crew Operations Directorate expressed opposition to a major effort to develop a lunar flyer until after the Apollo 16 mission. Plans for Apollo flights 12 through 16 required that the LM be maneuvered to landings at various points of scientific interest on the lunar surface, and experience from Apollo 11 and partial gravity simulators indicated the crews would be able to accomplish their surface EVA tasks for these missions without the aid of a mobility device.
References: 16.
1969 October 22 - -
Cosmonauts arrive in Moscow Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. The cosmonauts fly from Baikonur to Moscow, escorted by six MiG-21 fighters to Vnukovo airfield, where they receive honours all around, followed by meetings with reporters. Brezhnev was no there - he was on his way to Baikonur to observe the Tyulpan ICBM exercise.
References: 376.
1969 October 22 - 06:10 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 SL821. -
X-ray survey / Solar X X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 216 km (134 mi). References: 2.
1969 October 22 - 08:31 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 116 km (72 mi). References: 2.
1969 October 22 - 14:09 GMT - Launch Site: Baikonur. Launch Complex: LC81/24. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/D. LV Configuration: Proton-K/D 241-01. FAILURE: Block D control system failure. -
Cosmos 305 Nation: USSR. Program: Luna. Payload: Ye-8-5 s/n 404. Mass: 5,600 kg (12,300 lb). Class: Planetary. Type: Lunar. Spacecraft: Luna Ye-8-5. Agency: MOM. Perigee: 182 km (113 mi). Apogee: 208 km (129 mi). Inclination: 51.40 deg. Period: 88.40 min. COSPAR: 1969-092A. USAF Sat Cat: 4150. Decay Date: 1969-10-24. Robotic lunar soil return mission. Failed to leave low earth orbit due to Block D stage failure. References: 2, 6, 67, 274.
1969 October 23 - -
Czech delegation visits Baikonur Nation: USSR. A Czech delegation to Baikonur was shown the Vostok and Proton launch vehicles, Zenit-2, Ye-8, 7K-L1 spacecraft, a Vostok re-entry capsule, and the N1 moon launcher mock-up mounted on the remaining left launch pad. They were the first non-Russians to see evidence of the Russian manned lunar program. This was also Brezhnev's first view of Soviet moon-landing hardware. He proudly told the Czechs that 'this rocket will take us to the limits of the solar system'.
1969 October 23 - -
Cosmonauts feted at TsKBEM Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Traditional meeting between the cosmonauts and the engineers and workers at TsKBEM. They are quizzed on the flight failures, followed by dinner and toasts. Kamanin tells Afanasyev that instead of messing about with the N1-L3, they should build 8 to 10 more Soyuz and fly, fly, fly -- it is the only way to develop reliable systems. The Ministry of Defence needs a long-range plan of sustained flights of 5 to 6 spacecraft per year. All 300 present applaud the speech, except Mishin, who is against a new series of Soyuz spacecraft.
References: 376.
1969 October 23 - Launch Site: Baikonur. Launch Complex: LC161/35. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67P. LV Configuration: R-36 8K67P Palma-3. -
RVSN Command operational test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 23 - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Canopus. Model: Canopus 2. -
Test mission Nation: Argentina. Agency: IIAE. Apogee: 150 km (90 mi). References: 2.
1969 October 23 - 05:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 CRL A03.910-2. -
Infrared airglow profile Aurora infrared mission Nation: USA. Agency: AFCRL. Apogee: 190 km (110 mi). References: 2.
1969 October 24 - Launch Site: Baikonur. Launch Complex: LC142/34. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67P. LV Configuration: R-36 8K67P Palma-3. -
RVSN Command operational test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 24 - 05:44 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C S68/1. -
ESRO S68 / 1 X-ray astronomy mission Nation: Europe. Agency: ESRO. Apogee: 184 km (114 mi). References: 2.
1969 October 24 - 09:40 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 306 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 215 km (133 mi). Apogee: 299 km (185 mi). Inclination: 65.00 deg. Period: 89.60 min. COSPAR: 1969-093A. USAF Sat Cat: 4182. Duration: 12.00 days. Decay Date: 1969-11-05. Area survey photo reconnaissance satellite; returned film capsule. References: 2, 6.
1969 October 24 - 13:01 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/4. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 307 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 22. Mass: 250 kg (550 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 229 km (142 mi). Apogee: 2,150 km (1,330 mi). Inclination: 48.30 deg. Period: 109.20 min. COSPAR: 1969-094A. USAF Sat Cat: 4184. Completed Operations Date: 1970-11-11. Decay Date: 1970-12-30. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1969 October 24 - 18:10 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3B. LV Configuration: Titan 23B 23B-2 (3B-24). -
OPS 8455 Nation: USA. Payload: KH-8 no. 24 / Agena D. Mass: 3,000 kg (6,600 lb). Class: Surveillance. Type: Military. Spacecraft: KH-8. Agency: NRO/USAF. Perigee: 136 km (84 mi). Apogee: 740 km (450 mi). Inclination: 108.00 deg. Period: 93.40 min. COSPAR: 1969-095A. USAF Sat Cat: 4186. Decay Date: 1969-11-08. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1969 October 25 - Launch Site: Baikonur. Launch Complex: LC162/36. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67P. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 25 - 06:00 GMT - Launch Site: Resolute Bay. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3B. LV Configuration: Black Brant IIIB AKF-3B-50. -
Soft X-ray survey X-ray astronomy mission Nation: Canada. Agency: NRCC. Apogee: 192 km (119 mi). References: 2.
1969 October 26 - 06:40 GMT - Launch Site: Resolute Bay. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3B. LV Configuration: Black Brant IIIB AAF-3B-51. -
Soft X-ray survey X-ray astronomy mission Nation: Canada. Agency: NRCC. Apogee: 197 km (122 mi). References: 2.
1969 October 27 - -
HL-10 Flight 27 Nation: USA. Program: NASA Lifting Body. Payload: HL-10 flight 27. Class: Manned. Type: Spaceplane. Spacecraft: HL-10. Crew: Dana. Maximum Speed - 1675 kph. Maximum Altitude - 18470 m. Flight Time - 417 sec. References: 49, 97.
1969 October 27 - -
Cosmonauts tours. Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Kamanin assigns cosmonauts to upcoming foreign propaganda tours. Beregovoi and Feoktistov are to go to the United States, Tereshkova to Hungary, Popovich to France, Khrunov to Odessa. Titov will not be given this privilege because of his numerous automobile accidents, run-ins with the militia, and motorcycle habit.
References: 376.
1969 October 28 - -
Apollo lunar roving vehicle (LRV) contract awarded to the Boeing Nation: USA. Program: Apollo. Spacecraft: Apollo LRV. A lunar roving vehicle (LRV) cost-plus-incentive-fee contract was awarded to the Boeing Co. LRV-1 was scheduled for delivery on April 1, 1971, leaving only 17 months for vehicle development, production, and tests. The LRV project was managed at MSFC by Saverio F. Morea as a project within the Saturn Program Office. The Boeing Company would manage the LRV project in Huntsville, Ala., under Henry Kudish. General Motors Corp. AC Electronics Defense Research Laboratories in Santa Barbara, Calif., would furnish the mobility system (wheels, motors, and suspension). The Boeing Go. in Seattle, Wash., would furnish the electronics and navigation system. Vehicle testing would take place at the Boeing facility in Kent, Wash., and the chassis manufacturing and overall assembly would take place at the Boeing facility in Huntsville, Ala.
References: 16.
1969 October 29 - -
Titov wants out of the cosmonaut corps Nation: USSR. Titov wants out of the cosmonaut corps after hearing of his being banned from foreign travel. He is suffering a heavy penalty for his indiscretions. He has been banned from driving an automobile or flying an aircraft for two years, and lost his honoraria. References: 376.
1969 October 29 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Boosted Arcas. LV Configuration: Boosted Arcas NASA 15.42UI. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 110 km (60 mi). References: 2.
1969 October 29 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 29 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 29 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 29 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 29 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 29 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 29 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. -
Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 30 - 16:30 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3E. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 October 31 - -
Cosmonaut centre starved of equipment. Nation: USSR. Kamanin reviews the scandalous state of equipment deliveries to the cosmonaut centre. Only 10% of the equipment required by party decrees has been delivered, due to lack of support for manned spaceflight by the VVS. References: 376.
1969 October 31 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-304. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1969 November 1 - Launch Site: Baikonur. Launch Complex: LC90/20. Launch Pad: LC90/20?. Launch Vehicle: Tsiklon. Model: Tsiklon-2. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 200 km (120 mi). References: 2.
1969 November 2 - 20:20 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA CRL AJ17.602. -
Polar Cap U-2 Plasma mission Nation: USA. Agency: AFCRL. Apogee: 120 km (70 mi). References: 2.
1969 November 3 - -
HL-10 Flight 28 Nation: USA. Program: NASA Lifting Body. Payload: HL-10 flight 28. Class: Manned. Type: Spaceplane. Spacecraft: HL-10. Crew: Hoag. Maximum Speed - 1482kph. Maximum Altitude - 19540 m. Flight Time - 439 sec. References: 49, 97.
1969 November 3 - -
Apollo team made a walkaround inspection of Apollo 14 Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Flight: Apollo 14. The spacecraft walk-down team, established by ASPO in July in an effort to stem the increased number of human errors found in flight hardware, made a walkaround inspection of CSM-110 (Apollo 14 hardware). Cooperation of North American Rockwell and the Resident Apollo Spacecraft Program Office was excellent during the preparation and implementation of the inspection. No significant discrepancies were found by the inspection team during the several hours of inspection.
References: 16.
1969 November 3 - -
Press conference preparations Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8. A meeting is held with Mishin and Keldysh to prepare the cosmonauts and other participants for an upcoming press conference. Kamanin notes a huge amount of time is spent in such preparations. References: 376.
1969 November 3 - 06:05 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA CRL AJ17.758. -
Polar Cap U-1 Plasma mission Nation: USA. Agency: AFCRL. Apogee: 126 km (78 mi). References: 2.
1969 November 3 - 06:29 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.902-3. -
Polar Cap N-2 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 117 km (72 mi). References: 2.
1969 November 3 - 06:42 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AT07.396. -
Polar Cap C-1 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 210 km (130 mi). References: 2.
1969 November 3 - 07:30 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AG07.882. -
Polar Cap N-1 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 138 km (85 mi). References: 2.
1969 November 3 - 10:28 GMT - Launch Site: Resolute Bay. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3B. LV Configuration: Black Brant IIIB AAF-3B-48. -
Aurora / chemical release mission Nation: Canada. Agency: NRCC. Apogee: 200 km (120 mi). References: 2.
1969 November 3 - 12:32 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AT07.397. -
Polar Cap C-2 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 167 km (103 mi). References: 2.
1969 November 3 - 12:57 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. Model: Nike Javelin. -
BRL 2 Ionosphere / plasma mission Nation: USA. Agency: USAF. Apogee: 116 km (72 mi). References: 2.
1969 November 3 - 13:52 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA CRL AJ17.616. -
Polar Cap U-5 Plasma mission Nation: USA. Agency: AFCRL. Apogee: 113 km (70 mi). References: 2.
1969 November 3 - 16:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25C. Launch Pad: -. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3XD-8. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1969 November 3 - 17:11 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA CRL A17.906-1. -
Polar Ionosphere Ionosphere mission Nation: USA. Agency: AFCRL. Apogee: 126 km (78 mi). References: 2.
1969 November 3 - 17:30 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AH07.886. -
Polar Cap N-3 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 144 km (89 mi). References: 2.
1969 November 3 - 17:47 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.902-4. -
Polar Cap N-4 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 122 km (75 mi). References: 2.
1969 November 3 - 23:08 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AT07.398. -
Polar Cap C-4 Sphere Aeronomy mission Nation: USA. Agency: USAF. Apogee: 192 km (119 mi). References: 2.
1969 November 4 - Launch Site: Baikonur. Launch Complex: LC142/34. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67P. -
OS-67 No. 1L test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1969 November 4-7 -
1969 November 4 - 11:59 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63. -
Cosmos 308 Nation: USSR. Program: DS. Payload: DS-P1-I s/n 7. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-I. Agency: MO SSSR. Perigee: 271 km (168 mi). Apogee: 408 km (253 mi). Inclination: 71.00 deg. Period: 91.30 min. COSPAR: 1969-096A. USAF Sat Cat: 4219. Completed Operations Date: 1970-01-04. Decay Date: 1970-01-04. Operational radar target for the ABM forces. References: 2, 6, 99.
1969 November 4 - 19:29 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150 MI. LV Configuration: Aerobee 150 MI-20 NASA 04.136DS. -
NRL NE3.215 FDVU Solar extreme ultraviolet mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1969 November 4 - 20:27 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150 MI. LV Configuration: Aerobee 150 MI-20 NASA 04.283CS. -
Solar x-ray mission Nation: USA. Agency: NASA. Apogee: 181 km (112 mi). The rockets achieved expected performance, solar pointing systems functioned properly, payloads were successfully recovered, and preliminary results appeared excellent. The information obtained by the rocket flights on solar emission intensity, filter performance, film response, and exposure time would be available in time to provide a useful and effective feedback into the ATM instruments development program.
References: 2.
1969 November 4 - 22:38 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. Model: Nike Javelin. -
BRL 7 Ionosphere mission Nation: USA. Agency: USAF. Apogee: 125 km (77 mi). References: 2.
1969 November 4 - 22:50 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AH07.893. -
Polar Cap N-5 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 143 km (88 mi). References: 2.
1969 November 4 - 23:08 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA CRL AJ17.617. -
Polar Cap U-6 Plasma mission Nation: USA. Agency: AFCRL. Apogee: 126 km (78 mi). References: 2.
1969 November 5 - -
Press conference - lunar project raised. Nation: USSR. Program: Soyuz, Lunar L3. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Major press conference. Keldysh dodges questions from American reporters on the Soviet lunar landing program. The cosmonauts perform all right, no mistakes. Kamanin views Keldysh as a braking force on the space programme. He attributes the loss of the moon race to bad managers like Keldysh and Mishin.
References: 376.
1969 November 5 - 08:11 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 45.0 N x 46.0 W. Launch Vehicle: MR-12. -
Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 160 km (90 mi). References: 2.
1969 November 5 - 11:12 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 45.0 N x 46.0 W. Launch Vehicle: MR-12. -
Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 162 km (100 mi). References: 2.
1969 November 5 - 11:18 GMT - Launch Site: Resolute Bay. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3B. LV Configuration: Black Brant IIIB AAF-3B-49. -
Aurora / chemical release mission Nation: Canada. Agency: NRCC. Apogee: 200 km (120 mi). References: 2.
1969 November 5 - 20:49 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AH07.889. -
Polar Cap N? Aeronomy mission Nation: USA. Agency: USAF. Apogee: 122 km (75 mi). References: 2.
1969 November 6 - -
Cosmonaut photo sessions. Nation: USSR. Flight: Soyuz 6, Soyuz 7, Soyuz 8. The day is spent in photo sessions with the cosmonauts in various ministries. References: 376.
1969 November 6 - 20:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-209. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1969 November 7 - 02:51 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AH07.892. -
Polar Cap N-6 Aeronomy mission Nation: USA. Agency: USAF. Apogee: 122 km (75 mi). References: 2.
1969 November 7 - 07:00 GMT - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1225. -
ST Olympic TR. B-11 operational test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1969 November 8 - Launch Site: Kourou. Launch Complex: ALFS. Launch Pad: -. Launch Vehicle: Veronique. Model: Vesta. LV Configuration: Vesta 006. -
FU-189 Star pt test Nation: France. Agency: CNES. Apogee: 204 km (126 mi). References: 2.
1969 November 8 - 01:52 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout B. LV Configuration: Scout B S169C. -
Azur Nation: Germany. Payload: GRS A. Mass: 71 kg (156 lb). Class: Earth. Type: Magnetosphere. Spacecraft: AZUR. Agency: DFVLR. Perigee: 373 km (231 mi). Apogee: 2,127 km (1,321 mi). Inclination: 102.70 deg. Period: 110.50 min. COSPAR: 1969-097A. USAF Sat Cat: 4221. German Research Satellite A; examined Van Allen belts, solar particles, aurora. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1969 November 8 - 07:30 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB NRL NF9.207. -
Infrared astronomy mission Nation: USA. Agency: NRL. Apogee: 189 km (117 mi). References: 2.
1969 November 9 - 16:47 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 45.0 N x 46.0 W. Launch Vehicle: MR-12. -
Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 162 km (100 mi). References: 2.
1969 November 10 - -
Apollo 12 targetting point for Surveyor 3 changed Nation: USA. Program: Apollo. Spacecraft: Surveyor. Flight: Apollo 12. At the request of the Apollo 12 crew, the internal primary guidance and navigational control system targeting for descent was being changed so that the automatic guidance would land LM-6 at Surveyor III rather than at a point offset 305 meters east and 153 meters north as originally planned.
References: 16.
1969 November 10 - -
Associate Administrator for Manned Space Flight George E Mueller resigns Nation: USA. Program: Apollo. NASA announced the resignation of Associate Administrator for Manned Space Flight George E. Mueller effective December 10. In December Charles W. Mathews was named Acting Associate Administrator for Manned Space Flight until a successor for Mueller was appointed.
References: 16.
1969 November 10 - -
Cosmonauts in demand. Nation: USSR. Flight: Soyuz 6, Soyuz 7, Soyuz 8. Certain generals want the cosmonauts to appear at a meeting. Kamanin is forced to pull them out of follow-up physical examinations for the task. References: 376.
1969 November 10 - 21:00 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S46/1. -
ESRO S46 / 1 Aurora mission Nation: Europe. Agency: ESRO. Apogee: 214 km (132 mi). References: 2.
1969 November 12 - 11:30 GMT - Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 309 Nation: USSR. Payload: Zenit-2 11F61 s/n 80. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: MOM. Perigee: 185 km (114 mi). Apogee: 364 km (226 mi). Inclination: 64.50 deg. Period: 90.00 min. COSPAR: 1969-098A. USAF Sat Cat: 4223. Duration: 8.00 days. Decay Date: 1969-11-20. Area survey photo reconnaissance satellite. First flight with Nauka external experiment container. References: 2, 6,93.
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Nauka Nation: USSR. Payload: Nauka 3KS. Spacecraft: Nauka. Agency: MOM. Perigee: 188 km (116 mi). Apogee: 334 km (207 mi). Inclination: 65.40 deg. Period: 89.73 min. COSPAR: 1969-098E. USAF Sat Cat: 4236. Decay Date: 1969-11-30. References: 2, 279.
1969 November 13 - -
X-24 Flight 7 Nation: USA. Payload: X-24A flight 7. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Gentry. Glide. Maximum Speed - 687 kph. Maximum Altitude - 13720 m. Flight Time - 270 sec. References: 49, 97.
1969 November 14 - 16:22 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Saturn V. Model: Saturn V. LV Configuration: Saturn V SA-507. -
Apollo 12 Nation: USA. Program: Apollo. Payload: Apollo CSM 108 / Apollo LM 6 / ALSEP / S-IVB-507. Mass: 28,790 kg (63,470 lb). Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo CSM. Location of Spacecraft: Virginia Air and Space Center (NASA Langley Visitor's Center), Hampton, VA. Agency: NASA MSC. Perigee: 181 km (112 mi). Apogee: 186 km (115 mi). Inclination: 32.50 deg. Period: 88.19 min. COSPAR: 1969-099A. USAF Sat Cat: 4225. Duration: 10.19 days. Decay Date: 1969-11-24. Crew: Bean, Conrad, Gordon. Flight: Apollo 12. Apollo 12 (AS-507)-with astronauts Charles Conrad, Jr., Richard F. Gordon, Jr., and Alan L. Bean as the crewmen-was launched from Pad A, Launch Complex 39, KSC, at 11:22 a.m. EST November 14. Lightning struck the space vehicle twice, at 36.5 seconds and 52 seconds into the mission. The first strike was visible to spectators at the launch site. No damage was done. Except for special attention given to verifying all spacecraft systems because of the lightning strikes, the activities during earth-orbit checkout, translunar injection, and translunar coast were similar to those of Apollo 10 and Apollo 11.During the translunar coast astronauts Conrad and Bean transferred to the LM one-half hour earlier than planned in order to obtain full TV coverage through the Goldstone tracking station. The 56-minute TV transmission showed excellent color pictures of the CSM, the intravehicular transfer, the LM interior, the earth, and the moon. At 10:47 p.m. EST, November 17, the spacecraft entered a lunar orbit of 312.6 x 115.9 kilometers. A second service propulsion system burn circularized the orbit with a 122.5-kilometer apolune and a 100.6-kilometer perilune. Conrad and Bean again transferred to the LM, where they perfomed housekeeping chores, a voice and telemetry test, and an oxygen purge system check. They then returned to the CM. Conrad and Bean reentered the LM, checked out all systems, and at 10:17 p.m. EST on November 18 fired the reaction control system thrusters to separate the CSM 108 (the Yankee Clipper) from the LM-6 (the Intrepid). At 1:55 a.m. EST November 19, the Intrepid landed on the moon's Ocean of Storms, about 163 meters from the Surveyor III spacecraft that had landed April 19, 1967. Conrad, shorter than Neil Armstrong (first man on the moon, July 20), had a little difficulty negotiating the last step from the LM ladder to the lunar surface. When he touched the surface at 6:44 a.m. EST November 19, he exclaimed, "Whoopee! Man, that may have been a small step for Neil, but that's a long one for me." Bean joined Conrad on the surface at 7:14 a.m. They collected a 1.9-kilogram contingency sample of lunar material and later a 14.8-kilogram selected sample. They also deployed an S-band antenna, solar wind composition experiment, and the American flag. An Apollo Lunar Surface Experiments Package with a SNAP-27 atomic generator was deployed about 182 meters from the LM. After 3 hours 56 minutes on the lunar surface, the two astronauts entered the Intrepid to rest and check plans for the next EVA. The astronauts again left the LM at 10:55 p.m. EST November 19. During the second EVA, Conrad and Bean retrieved the lunar module TV camera for return to earth for a failure analysis, obtained photographic panoramas, core and trench samples, a lunar environment sample, and assorted rock, dirt, bedrock, and molten samples. The crew then examined and retrieved parts of Surveyor III, including the TV camera and soil scoop. After 3 hours 49 minutes on the lunar surface during the second EVA, the two crewmen entered the LM at 2:44 a.m. EST November 20. Meanwhile astronaut Gordon, orbiting the moon in the Yankee Clipper, had completed a lunar multispectral photography experiment and photographed proposed future landing sites. At 9:26 a.m. EST November 20, after 31 hours 31 minutes on the moon, Intrepid successfully lifted off with 34.4 kilograms of lunar samples. Rendezvous maneuvers went as planned. The LM docked with the CSM at 12:58 p.m. November 20. The last 24 minutes of the rendezvous sequence was televised. After the crew transferred with the samples, equipment, and film to the Yankee Clipper, the Intrepid was jettisoned and intentionally crashed onto the lunar surface at 5:17 p.m. November 20, 72.2 kilometers southeast of Surveyor III. The crash produced reverberations that lasted about 30 minutes and were detected by the seismometer left on the moon. At 3:49 p.m. EST November 21, the crew fired the service propulsion system engine, injecting the CSM into a transearth trajectory after 89 hours 2 minutes in lunar orbit. During the transearth coast, views of the receding moon and the interior of the spacecraft were televised, and a question and answer session with scientists and the press was conducted.
References: 2, 6, 16, 26, 27, 33,60.
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Apollo 12 LM Nation: USA. Program: Apollo. Payload: Apollo LM 6. Mass: 15,223 kg (33,560 lb). Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo LM. Agency: NASA MSC. Perigee: 181 km (112 mi). Apogee: 186 km (115 mi). Inclination: 32.50 deg. Period: 88.19 min. COSPAR: 1969-099x. USAF Sat Cat: 4225. Duration: 10.19 days. Decay Date: 1969-11-24. Flight: Apollo 12. References: 2, 6, 16, 26, 27, 33,60.
1969 November 15 - 08:30 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57. -
Cosmos 310 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 336 km (208 mi). Inclination: 65.00 deg. Period: 89.90 min. COSPAR: 1969-100A. USAF Sat Cat: 4232. Duration: 8.00 days. Decay Date: 1969-11-23. High resolution photo reconnaissance satellite; returned film capsule References: 2, 6.
1969 November 15 - 17:00 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2E. LV Configuration: Polaris A2E A2E. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1969 November 16 - Launch Site: Jiuquan. Launch Complex: LA2A. Launch Pad: -. Launch Vehicle: CZ-1. Model: CZ-1. FAILURE: The program distributor in the second stage broke down. The rocket crashed into the earth within view of the launch site after 69 seconds of flight. -
First Chinese satellite launch attempt ends in failure. Nation: China. Payload: DFH 1. Mass: 170 kg (370 lb). Class: Technology. Spacecraft: DFH-1. COSPAR: F691116Z. The launch vehicle arrived at the site on 18 March 1969. The objective was to launch China's first satellite before Japan lofted its counterpart. Ren Xinmin had obtained this specific order from Deng Hsiao Peng. Great difficulties were encountered in the middle of the Cultural Revolution, including the sending of most of the satellite engineers to work on irrigation ditch construction in the provinces. The skirt for the satellite, designed to make it easily visible to ground observors, had to be made from a special silk produced in a factory without the knowledge of the Red Guards. The engineers went by bus to a department store in Beijing to study an imported folding umbrella as a model for the deployment mechanism -- they could not afford to buy it. The entire launch was kept secret until a documentary was released in 2001.
References: 5.
1969 November 17 - -
HL-10 Flight 29 Nation: USA. Program: NASA Lifting Body. Payload: HL-10 flight 29. Class: Manned. Type: Spaceplane. Spacecraft: HL-10. Crew: Dana. Maximum Speed - 1693 kph. Maximum Altitude - 19690 m. Flight Time - 408 sec. References: 49, 97.
1969 November 17 - -
Changed nomenclature for the lunar exploration phase of the Apollo program Nation: USA. Program: Apollo. Flight: Apollo 11. NASA discontinued the use of names such "LEO," "ALEM," and "Apollo Lunar Exploration Program" that had been used since Apollo 11 to identify the lunar exploration phase of the Apollo program. Henceforth, the single word title "Apollo" would be used when referring to the program.
Additional Details: Changed nomenclature for the lunar exploration phase of the Apollo program. References: 16.
1969 November 18 - 02:17 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL602. FAILURE: Failure. -
Fresnel shadowgraph X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 208 km (129 mi). References: 2.
1969 November 18 - 03:47 GMT - -
Apollo 12 enters lunar orbit Nation: USA. Flight: Apollo 12. At 03:47 GMT November 18 Apollo 12 arrived at the moon 83 1/2 hours after liftoff. Conrad fired the main propulsion engine for almost 6 minutes to go into an elliptical lunar orbit. Five hours later a second burn put the spacecraft into a circular orbit at 60 nautical miles (111 kilometers) altitude, where Yankee Clipper would stay until it was time to return to earth.
Additional Details: Apollo 12 enters lunar orbit.
1969 November 18 - 13:34 GMT - Launch Site: Biscarosse. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 3. LV Configuration: Dragon 3 D-304. -
FU-192 Plasma Ionosphere mission Nation: France. Agency: CNES. Apogee: 475 km (295 mi). References: 2.
1969 November 18 - 21:32 GMT - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-12 Sandia 152-135. -
LRL ACS-5 Solar x-ray mission Nation: USA. Agency: Sandia. Apogee: 174 km (108 mi). References: 2.
1969 November 19 - Launch Site: Vandenberg. Launch Complex: LF21. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2508. -
ST Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1969 November 19 - 06:55 GMT - -
Apollo 12 makes a precision landing on the lunar surface Nation: USA. Flight: Apollo 12. Conrad and Bean reentered the LM, checked out all systems, and at 10:17 p.m. EST on November 18 fired the reaction control system thrusters to separate the CSM 108 (the Yankee Clipper) from the LM-6 (the Intrepid). At 1:55 a.m. EST November 19, the Intrepid landed on the moon's Ocean of Storms, about 163 meters from the Surveyor III spacecraft that had landed April 19, 1967.
Additional Details: Apollo 12 makes a precision landing on the lunar surface.
1969 November 19 - 11:32 GMT - -
EVA Apollo 12-1 Nation: USA. Program: Apollo. Class: Manned. Type: Lunar lander. Spacecraft: Apollo LM. Crew: Conrad, Bean. Flight: Apollo 12. EVA Duration: 0.16 days. Explored lunar surface near LM and deployed ALSEP unmanned scientific station equipment. References: 66.
1969 November 20 - -
EVA Apollo 12-3 Nation: USA. Program: Apollo. Class: Manned. Type: Lunar lander. Spacecraft: Apollo LM. Crew: Conrad, Bean. Flight: Apollo 12. EVA Duration: 0.0014 days. Threw excess equipment out of LM before lift-off. References: 66.
1969 November 20 - 00:30 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL801. -
Solar ultraviolet Spectrum / PHC Solar ultraviolet and x-ray mission Nation: UK. Agency: BAC. Apogee: 242 km (150 mi). References: 2.
1969 November 20 - 03:54 GMT - -
EVA Apollo 12-2 Nation: USA. Program: Apollo. Class: Manned. Type: Lunar lander. Spacecraft: Surveyor. Crew: Conrad, Bean. Flight: Apollo 12. EVA Duration: 0.16 days. Moonwalk to Surveyor 3, which had landed two years before. Recovered parts of Surveyor 3 which seemed to show that Earth bacteria could survive for that period in space and be revived. References: 66.
1969 November 21 - -
HL-10 Flight 30 Nation: USA. Program: NASA Lifting Body. Payload: HL-10 flight 30. Class: Manned. Type: Spaceplane. Spacecraft: HL-10. Crew: Hoag. Maximum Speed - 1532 kph. Maximum Altitude - 24160 m. Flight Time - 378 sec. References: 49, 97.
1969 November 21 - -
Apollo 12 heads for home Nation: USA. Flight: Apollo 12. At 3:49 p.m. EST November 21, the crew fired the service propulsion system engine, injecting the CSM into a transearth trajectory after 89 hours 2 minutes in lunar orbit. During the transearth coast, views of the receding moon and the interior of the spacecraft were televised, and a question and answer session with scientists and the press was conducted.
Additional Details: Apollo 12 heads for home.
1969 November 22 - 00:37 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta M. LV Configuration: Thor Delta M 554/D74. -
Skynet 1A Nation: UK. Program: Skynet. Mass: 243 kg (535 lb). Class: Communications. Type: Military. Spacecraft: NATO 1. Agency: UK MoD. Perigee: 35,682 km (22,171 mi). Apogee: 35,894 km (22,303 mi). Inclination: 13.90 deg. Period: 1,436.20 min. COSPAR: 1969-101A. USAF Sat Cat: 4250. Completed Operations Date: 1980-01-01. Over Indian Ocean. Military communications. Previously registere
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