Encyclopedia Astronautica
October 29


October 29 Chronology


1935 October 29 - . LV Family: Goddard. Launch Vehicle: Goddard A.
  • Flight of Goddard A series rocket - . Nation: USA. Related Persons: Goddard. Apogee: 1.22 km (0.76 mi). Rocket had new gasoline orifices; duration of lift 12 sec; altitude about 4000 ft; speed high -- shot a wave of dirt, resembling a water wave, before it on landing. This completed Goddard's test of the A series of rockets. They had included 10 proving-stand tests and 14 flight test attempts, of which 7 resulted in flights. Average interval between tests was 28 days

1944 October 29 - . Launch Site: Heidekraut. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 19486.
  • V-2 Ma242 208 J2 - . Nation: Germany. Summary: Planned range 225 km. Accuracy 5.4 km to the right of the planned trajectory. Circular error 5.5 km from aim point..

1947 October 29 - .
  • XS-1 Flight 54 - . Crew: Yeager. Payload: XS-1 # 1 flight 34. Nation: USA. Related Persons: Yeager. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: AF flight 12. Telemetry failure..

1951 October 29 - . 21:04 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 60.
  • Probe Aeronomy mission - . Nation: USA. Apogee: 137 km (85 mi). Summary: Launched 14:04 local time. Reached 141.3 km. Carried pressure, temperature experiments for Signal Corps Engineering Lab, University of Michigan..

1952 October 29 - .
  • Birth of Valeri Ivanovich Tokarev - . Nation: Russia. Summary: Russian test pilot cosmonaut. Flew on STS-96, ISS EO-12. Russian Air Force test pilot, flying 44 types of aircraft and helicopters. Selected as Buran test pilot in 1987. From 1994, commander cosmonaut group for aerospace systems..

1952 October 29 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1 8A11. LV Configuration: R-1 8A11 No 420.
  • Operational test - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1954 October 29 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bechar. LV Family: Veronique. Launch Vehicle: Veronique. LV Configuration: Veronique NA12.
  • Test mission - . Nation: France. Agency: LRBA. Apogee: 90 km (55 mi).

1957 October 29 - . 00:13 GMT - . Launch Site: Pacific Ocean. Launch Pad: 50.7 S x 169.7 W. Launch Platform: AGB-4. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon SUI 94.
  • II5.70F Aeronomy / Chemical release mission - . Nation: USA. Agency: SUI. Apogee: 100 km (60 mi).

1959 October 29 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC22. LV Family: Mace. Launch Vehicle: Mace. LV Configuration: Mace 56-2884.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1959 October 29 - . 02:12 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC18B. Launch Pad: LC18B. LV Family: Delta. Launch Vehicle: Thor DM-18A. LV Configuration: Thor DM-18A 230.
  • Series IV research and development launch/Meteorites mission - . Nation: USA. Agency: USAF. Apogee: 520 km (320 mi).

1959 October 29 - . 07:20 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 26D.
  • Research and development test - . Nation: USA. Agency: USAF. Apogee: 1,800 km (1,100 mi). Summary: USAF Atlas successfully launched from Cape Canaveral carrying a nose-cone camera which took a series of photographs of the earth's cloud cover from a 300-mile altitude..

1961 October 29 - .
  • U.S.S.R. fires 50-megaton hydrogen bomb, biggest explosion in history - . Nation: USSR.

1961 October 29 - .
  • Mercury-Scout launch announced. - . Nation: USA. Program: Mercury. Class: Technology. Type: Tracking network technology satellite. Spacecraft: Radio Test Spacecraft. Summary: NASA announced that first Mercury-Scout launch to verify the readiness of the worldwide Mercury tracking network would take place at Atlantic Missile Range..

1961 October 29 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/4. Launch Pad: LC41?/pad?. LV Family: R-16. Launch Vehicle: R-16.
  • K (OT) test - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1962 October 29 - . Launch Site: Barking Sands. LV Family: Honest John. Launch Vehicle: HJ Nike.
  • Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 100 km (60 mi).

1962 October 29 - . 23:21 GMT - . Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. LV Family: Veronique. Launch Vehicle: Veronique. LV Configuration: Veronique AGI34.
  • Aeronomy /ionosphere mission - . Nation: France. Agency: CNES. Apogee: 180 km (110 mi).

1963 October 29 - .
  • The issue of the Nikolayev/Tereshkova wedding has come to a head. - . Nation: USSR. Related Persons: Nikolayev; Tereshkova. The wedding has to be arranged with the VVS General Staff in accordance with the resolution of the Central Committee. Kamanin calls Tereshkova and Nikolayev and orders them to decide the issue - the MUST SET A DATE. He is getting ten phone calls a day about it and can resist no longer.

1963 October 29 - . 02:53 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 2. LV Configuration: Black Brant II CC-2A-40.
  • NO2 release Aeronomy mission - . Nation: Canada. Agency: CARDE. Apogee: 140 km (80 mi).

1963 October 29 - . 20:42 GMT - . Launch Site: Hidden Hills DZ. Launch Pad: 36.1 N x 116.0 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 1-40-64.
  • X-15A Checkout/Opt Deg. Test/Technology mission - . Nation: USA. Agency: NASA; USAF. Apogee: 22 km (13 mi). Summary: Maximum Speed - 4364 kph. Maximum Altitude - 22600 m..

1963 October 29 - . 21:19 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1W. LV Family: Delta. Launch Vehicle: Thor Agena D SLV-2A/D. LV Configuration: Thor SLV-2A Agena D 386 / Agena D 1601.
  • KH-5 9059A - . Payload: KH-5 s/n 9059A/Agena D 1601. Mass: 1,500 kg (3,300 lb). Nation: USA. Agency: NRO; CIA. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-5. Decay Date: 1964-01-21 . USAF Sat Cat: 681 . COSPAR: 1963-042A. Apogee: 318 km (197 mi). Perigee: 283 km (175 mi). Inclination: 89.9000 deg. Period: 90.60 min. Summary: KH-5; deployed ELINT subsatellite. Fourth film payload retrieved in ARGON program. Film comparable to that of 9058A. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
  • Hitch Hiker 2 - . Payload: P-11 s/n A3. Mass: 80 kg (176 lb). Nation: USA. Agency: NRO; USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: SSF. Decay Date: 1965-05-23 . USAF Sat Cat: 682 . COSPAR: 1963-042B. Apogee: 581 km (361 mi). Perigee: 288 km (178 mi). Inclination: 90.0000 deg. Period: 93.30 min. Summary: Radar monitoring..

1964 October 29 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 450.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 October 29 - . 01:59 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/22. LV Family: Tsiklon. Launch Vehicle: R-36 8K67.
  • Kura state trials missile launch - . Nation: USSR. Agency: RVSN. Apogee: 868 km (539 mi).

1964 October 29 - . 03:35 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Delta. Launch Vehicle: Thor DSV-2F. LV Configuration: Thor DSV-2F 260.
  • ASSET 4 re-entry vehicle test flight - . Nation: USA. Agency: USAF. Apogee: 50 km (31 mi). Suborbital test of small scale spaceplane model to test structural concepts for the X-20 Dynasoar. Aero-environmental test vehicle (AEV) to test aerodynamic properties of flexing outer skin with corrugated columbium panel. Reached 4,000 m/s at 50.6 km altitude before being released from launch vehicle. Telemetry received for 900 seconds until spaceplane had reached Mach 2 1200 km downrange. It then became unstable and crashed into the Atlantic. Recovery was not planned.

1964 October 29 - . 23:18 GMT - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Belier. Launch Vehicle: Centaure.
  • ESRO C02 / 1 Aeronomy mission - . Nation: Europe. Agency: ESRO. Apogee: 150 km (90 mi).

1965 October 29 - . Launch Site: Baikonur. Launch Complex: Baikonur PU33. LV Family: Tsiklon. Launch Vehicle: R-36 8K67.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1965 October 29 - . 11:30 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NRL NF3.162R.
  • Infrared Telescope Infrared astronomy mission - . Nation: USA. Agency: NRL. Apogee: 205 km (127 mi).

1967 October 29 - . LV Family: N1. Launch Vehicle: N1.
  • Cosmos 188 launch scrubbed. - . Nation: USSR. Program: Soyuz; Lunar L3. Spacecraft: Soyuz 7K-OK. The Soyuz-B ('Baikal') launch was delayed to 30 October due to problems with the celestial navigation system aboard Cosmos 186. Later that day an N1-L3 review is held. The first launch vehicle will be completed in two to three weeks, but the launch complex will not be ready until next January. The first trials of the booster on the pad will begin in February-March 1968, with the first launch in the second half of the year.

1968 October 29 - . 11:32 GMT - . Launch Site: Johnston Island. Launch Complex: Johnston Island UL6. LV Family: Sandhawk. Launch Vehicle: Terrier Sandhawk. LV Configuration: Terrier Sandhawk Sandia 281-10.
  • LRL ACS-3 X-ray astronomy mission - . Nation: USA. Agency: Sandia. Apogee: 320 km (190 mi).

1969 October 29 - .
  • Titov wants out of the cosmonaut corps - . Nation: USSR. Related Persons: Titov. Summary: 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..

1969 October 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 601. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1969 October 29 - . Launch Site: Wallops Island. LV Family: Arcas. Launch Vehicle: Boosted Arcas. LV Configuration: Boosted Arcas NASA 15.42UI.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 110 km (60 mi).

1969 October 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 601. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1969 October 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 601. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1969 October 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 601. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1969 October 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 601. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1969 October 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 601. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1969 October 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 601. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1970 October 29 - . Launch Site: Baikonur. Launch Complex: Baikonur LC142/34. LV Family: Tsiklon. Launch Vehicle: R-36 8K67.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 October 29 - . 21:39 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna S. LV Family: Skylark. Launch Vehicle: Skylark 2. LV Configuration: Skylark 2 S67/2.
  • ESRO S67 / 2 Aurora mission - . Nation: Europe. Agency: ESRO. Apogee: 234 km (145 mi).

1971 October 29 - . 10:09 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 CRL A04.004-5.
  • HISTAR 3 Infrared astronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 158 km (98 mi).

1972 October 29 - . 15:48 GMT - . Launch Site: Andoya. LV Family: Skua. Launch Vehicle: Skua 2. LV Configuration: Skua 2 SK21A.
  • Ionosphere / barium release mission - . Nation: UK. Agency: SRC. Apogee: 100 km (60 mi).

1973 October 29 - . 14:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Vostok 8A92M.
  • Cosmos 604 - . Payload: Tselina-D no. 5. Mass: 2,000 kg (4,400 lb). Nation: USSR. Agency: MOM. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. Decay Date: 1992-01-19 . USAF Sat Cat: 6907 . COSPAR: 1973-080A. Apogee: 424 km (263 mi). Perigee: 413 km (256 mi). Inclination: 81.2000 deg. Period: 92.90 min.

1974 October 29 - . 19:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Titan. Launch Vehicle: Titan 3D. LV Configuration: Titan IIID 23D-4.
  • KH-9 no. 09 - . Mass: 13,300 kg (29,300 lb). Nation: USA. Agency: NRO; CIA. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-9. Decay Date: 1975-03-18 . USAF Sat Cat: 7495 . COSPAR: 1974-085A. Apogee: 272 km (169 mi). Perigee: 115 km (71 mi). Inclination: 96.7000 deg. Period: 88.40 min. Summary: KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OPS 6239 - . Payload: SSF-B No. 26. Mass: 60 kg (132 lb). Nation: USA. Agency: NRO; USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: SSF. Decay Date: 1980-01-23 . USAF Sat Cat: 7498 . COSPAR: 1974-085B. Apogee: 531 km (329 mi). Perigee: 521 km (323 mi). Inclination: 96.0000 deg. Period: 95.10 min. Summary: Radar monitoring; may or may not have existed!!!..
  • SESP 73-5 - . Payload: P 73 5 / OPS 8452. Nation: USA. Agency: USAF. Class: Technology. Type: Military technology satellite. Spacecraft: SESP. Decay Date: 1975-05-26 . USAF Sat Cat: 7499 . COSPAR: 1974-085C. Apogee: 2,888 km (1,794 mi). Perigee: 150 km (90 mi). Inclination: 96.9000 deg. Period: 116.30 min. Summary: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1975 October 29 - . 02:39 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170A. LV Configuration: Aerobee 170A NASA 13.48GG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 186 km (115 mi).

1975 October 29 - . 11:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 777 - . Mass: 3,000 kg (6,600 lb). Nation: USSR. Agency: MO. Program: EORSAT. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: US-P. Decay Date: 1976-06-03 . USAF Sat Cat: 8416 . COSPAR: 1975-102A. Apogee: 442 km (274 mi). Perigee: 425 km (264 mi). Inclination: 65.0000 deg. Period: 93.30 min. Summary: Ocean monitoring; exploded 1/76..

1975 October 29 - . 14:28 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy/Ionosphere/Chemical release/Plasma mission - . Nation: USSR. Apogee: 164 km (101 mi).

1976 October 29 - .
  • Complete Delta F retest, Enterprise (OV-101) - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise.

1976 October 29 - . Launch Site: Sary Shagan. Launch Vehicle: S-225.
  • Intercept - . Nation: USSR. Agency: PKO. Apogee: 180 km (110 mi).

1976 October 29 - . 12:40 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53772-414.
  • Cosmos 864 - . Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 9509 . COSPAR: 1976-108A. Apogee: 1,005 km (624 mi). Perigee: 958 km (595 mi). Inclination: 82.9000 deg. Period: 104.70 min. Summary: Military navigation satellite..

1976 October 29 - . 22:11 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.155UA.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 123 km (76 mi).

1977 October 29 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission? - . Nation: USSR. Agency: AN. Apogee: 150 km (90 mi).

1978 October 29 - . 05:02 GMT - . Launch Site: Poker Flat. LV Family: Super Chief. Launch Vehicle: Talos Castor. LV Configuration: Talos Castor DNA EX851.44-1.
  • EXCEDE 1 Active plasma mission - . Nation: USA. Agency: USAF GL. Apogee: 137 km (85 mi).

1979 October 29 - . 15:22 GMT - . Launch Site: Thule AFB. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 69 km (42 mi).

1980 October 29 - . 02:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 90 km (55 mi).

1982 October 29 - . 21:59 GMT - . Launch Site: Eareckson. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 49 km (30 mi).

1983 October 29 - . 08:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 1507 - . Mass: 3,000 kg (6,600 lb). Nation: USSR. Agency: MO. Program: EORSAT. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: US-P. Decay Date: 1987-08-19 . USAF Sat Cat: 14455 . COSPAR: 1983-110A. Apogee: 325 km (201 mi). Perigee: 298 km (185 mi). Inclination: 65.0000 deg. Period: 90.80 min. Summary: Ocean monitoring..

1984 October 29 - . 21:27 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 72 km (44 mi).

1985 October 29 - . 15:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 60 km (37 mi).

1986 October 29 - . 15:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 63 km (39 mi).

1987 October 29 - . 14:30 GMT - . Launch Site: Ascension. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 53 km (32 mi).

1988 October 29 - . LV Family: Energia. Launch Vehicle: Energia.
  • Buran first launch attempt - . Nation: USSR. Spacecraft: Buran. 51 seconds before the launch, when control of the countdown switched to automated systems, a software problem led the computer program to abort the lift-off. The problem was found to be due to late separation of a gyro update umbilical. The software problem was rectified and the next attempt was set for 15 November at 06:00 (03:00 GMT).

1990 October 29 - . 15:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 66 km (41 mi).

1991 October 29 - .
  • Galileo, Asteroid Gaspra Flyby - . Nation: USA. Spacecraft: Galileo.

1991 October 29 - . 23:08 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L V47.
  • Intelsat 6A F-1 - . Payload: Intelsat 601. Mass: 4,330 kg (9,540 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 393. USAF Sat Cat: 21765 . COSPAR: 1991-075A. Apogee: 35,791 km (22,239 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.0000 deg. Period: 1,436.20 min. International communications; 27.5 deg W. Positioned in geosynchronous orbit at 27 deg W in 1992-1997; 34 deg W in 1997-1999 As of 2 September 2001 located at 34.48 deg W drifting at 0.002 deg W per day. As of 2007 Mar 10 located at 63.65E drifting at 0.000W degrees per day.

1992 October 29 - . 10:40 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC133/3. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65078-424.
  • Cosmos 2218 - . Mass: 825 kg (1,818 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 22207 . COSPAR: 1992-073A. Apogee: 1,014 km (630 mi). Perigee: 967 km (600 mi). Inclination: 82.9000 deg. Period: 104.90 min. Summary: Military navigation satellite. Positioned in plane 3 of constellation..

1993 October 29 - . 13:38 GMT - .
1995 October 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 727. LV Family: Trident. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 DASO-34.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1996 October 29 - . 03:30 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.149UL.
1997 October 29 - .
  • Iraq expels all U.S. members of UN arms-inspection team - . Nation: International.

1998 October 29 - . 19:19 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39B. LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-95.
  • STS-95 - . Call Sign: Discovery. Crew: Brown; Lindsey; Robinson; Parazynski; Duque; Mukai; Glenn. Payload: Discovery F25. Nation: USA. Related Persons: Brown; Lindsey; Robinson; Parazynski; Duque; Mukai; Glenn. Agency: NASA Houston. Manufacturer: Douglas. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-95. Spacecraft: Discovery. Duration: 8.91 days. Decay Date: 1998-11-07 . USAF Sat Cat: 25519 . COSPAR: 1998-064A. Apogee: 557 km (346 mi). Perigee: 536 km (333 mi). Inclination: 28.5000 deg. Period: 95.60 min. The flight of STS-95 provoked more publicity for NASA than any other flight in years, due to the presence of ex-astronaut Senator John Glenn on the crew, which also included the first Spanish astronaut, Pedro Duque. The US Navy PANSAT student satellite was deployed on Oct 30 into a 550 km x 561 x 28.5 degree orbit. The Spartan 201 satellite was deployed from Discovery on November 1 and retrieved on November 3. Spartan 201 was on its fifth mission to observe the solar corona. The data on this mission would be used to recalibrate the SOHO satellite which recently resumed observation of the Sun following loss of control. Discovery landed at 17:03:31 GMT November 7 on Runway 33 at the Shuttle Landing Facility at Kennedy Space Center.
  • Spacehab - . Nation: USA. Agency: NASA Houston. Manufacturer: Douglas. Program: STS. Class: Manned. Type: Manned space laboratory. Spacecraft: Spacehab. Decay Date: 1981-04-13 . USAF Sat Cat: 25519 . COSPAR: 1998-064xx. Apogee: 560 km (340 mi). Perigee: 550 km (340 mi). Inclination: 28.4000 deg. Period: 95.75 min.
  • Spartan 201 - . Nation: USA. Agency: NASA Greenbelt. Program: STS. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: Spartan. Decay Date: 1998-11-07 . USAF Sat Cat: 25521 . COSPAR: 1998-064C. Apogee: 560 km (340 mi). Perigee: 549 km (341 mi). Inclination: 28.4000 deg. Period: 95.74 min. Summary: Retrieved by Discovery November 3 1998..

2000 October 29 - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP-3 V134.
  • EuropeStar F1 - . Payload: Europe*Star FM1. Mass: 4,167 kg (9,186 lb). Nation: UK. Agency: EuropeSt. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 26590 . COSPAR: 2000-068A. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. 100th Ariane 4 launch. Communications satellite, stationed at 45 deg E. Europeon.Star FM1 was a Loral FS-1300 model with a launch mass of 4167 kg and a dry mass of 1717 kg. The satellite had two cruciform solar arrays. The Ariane booster placed it into a geostationary transfer orbit. Positioned in geosynchronous orbit at 45 deg E in 2000. As of 4 September 2001 located at 44.95 deg E drifting at 0.011 deg E per day. As of 2007 Feb 23 located at 44.97E drifting at 0.001W degrees per day.

2002 October 29 - .
  • International Space Station Status Report #02-48 - . Nation: USA. Related Persons: Korzun; Lonchakov; Whitson; Zalyotin. Program: ISS. Flight: ISS EO-5. Right on time, a Russian-Belgian cosmonaut crew blasted off in a newly modified Soyuz capsule from the Baikonur Cosmodrome in Kazakhstan tonight, headed for a linkup to the International Space Station later this week to deliver a fresh crew return vehicle. Additional Details: International Space Station Status Report #02-48.

2004 October 29 - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M 410-08.
  • Ekspress AM-1 - . Mass: 2,542 kg (5,604 lb). Nation: Russia. Agency: ILS. Class: Communications. Type: Civilian communications satellite. Spacecraft: Ekspress. USAF Sat Cat: 28463 . COSPAR: 2004-043A. Apogee: 35,792 km (22,240 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Russian Satellite Communications Company spacecraft, to be stationed at 40 deg E, providing 28 C, Ku, and L band transponders for a wide range of communications and data services. The Ekspress-AM uses an improved Ekspress-M or 727M bus, first used on the Sesat satellite, while the earlier models used the KAUR-4 MSO-2500 bus. As of 2007 Mar 10 located at 39.98E drifting at 0.006W degrees per day.

2007 October 29 - .
2008 October 29 - . 16:54 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3B. LV Configuration: CZ-3B s/n CZ3B11.
  • Simon Bolivar - . Mass: 5,100 kg (11,200 lb). Nation: Venezuela. Agency: SISE. Class: Communications. Type: Civilian communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 33414 . COSPAR: 2008-055A. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.2000 deg. Period: 1,436.10 min. Summary: Venezuela's first satellite, a Chinese-built DFH-4 communications satellit with C-band and Ku-band transponders..

2009 October 29 - . 20:00 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • NSS 12 - . Mass: 5,620 kg (12,380 lb). Nation: France. Agency: Arianespace. Program: Intelsat. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 36032 . COSPAR: 2009-058A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: C- and Ku-band communications satellite stationed at 57 deg E..
  • Thor 6 - . Payload: Spacebus 4000B2. Mass: 3,050 kg (6,720 lb). Nation: France. Agency: Arianespace. Program: Thor Comsat. Class: Communications. Type: Communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 36033 . COSPAR: 2009-058B. Apogee: 35,793 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Direct broadcast satellite stationed at 1 deg W..

2010 October 29 - . 02:10 GMT - . Launch Site: White Sea Launch Area. Launch Platform: TK-208. LV Family: Bulava. Launch Vehicle: Bulava.
  • RV x 3 - . Nation: Russia. Apogee: 1,000 km (600 mi). Summary: R&D test..

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