Encyclopedia Astronautica
October 16


October 16 Chronology


1944 October 16 - . 15:30 GMT - . Launch Site: V-2 Battery 444. LV Family: V-2. Launch Vehicle: V-2.
  • V-2 combat launch from Rijsterbos - . Nation: Germany. Summary: Rijsterbos, Middenleane, rocket fired, impact unknown..

1945 October 16 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Wac. Launch Vehicle: WAC A. LV Configuration: WAC A 7.
  • Test mission - . Nation: USA. Agency: USA OR. Apogee: 27 km (16 mi).

1947 October 16 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike G.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1951 October 16 - . Launch Site: Holloman. Launch Complex: Holloman SLED. LV Family: Snark. Launch Vehicle: MX-775.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 10 km (6 mi).

1953 October 16 - . 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 820.
  • Operational test - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1956 October 16 - .
  • Birth of Dr James Hansen 'Jim' Newman - . Nation: USA. Summary: American physicist mission specialist astronaut. Flew on STS-51, STS-69, STS-88, STS-109..

1957 October 16 - . 20:02 GMT - . Launch Site: Pacific Ocean. Launch Pad: 7.1 N x 156.6 W. Launch Platform: AGB-4. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon II5.55F.
  • SUI 79 Aeronomy / Fields mission - . Nation: USA. Agency: SUI. Apogee: 100 km (60 mi).

1958 October 16 - .
  • X-1E Flight 25 - . Crew: McKay. Payload: X-1E flight 25. Nation: USA. Related Persons: McKay. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1E. Summary: NACA flight 24. First flight with elevated chamber pressure; cut short because overcast obscured pilot's view of lakebed..

1958 October 16 - . Launch Site: Sary Shagan. Launch Complex: Sary Shagan LC6. Launch Vehicle: V-1000.
  • State trials missile test - . Nation: USSR. Agency: PKO. Apogee: 15 km (9 mi).

1959 October 16 - . 11:17 GMT - . Launch Site: Eglin. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun AA6.215C.
  • Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 139 km (86 mi).

1960 October 16 - . Launch Site: ETR Launch Area. Launch Pad: 500NM. Launch Platform: SSBN 599. LV Family: Polaris. Launch Vehicle: Polaris A1. LV Configuration: Polaris A1FP-7.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1961 October 16 - . 14:54 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 608. LV Family: Polaris. Launch Vehicle: Polaris A1. LV Configuration: Polaris A1E-38.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1962 October 16 - . Launch Site: Baikonur. Launch Complex: Baikonur LC60/8. Launch Pad: LC60/8?. LV Family: R-16. Launch Vehicle: R-16U.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1962 October 16 - . 09:14 GMT - . Launch Site: Johnston Island. Launch Complex: Johnston Island LE2. LV Family: Delta. Launch Vehicle: Thor DSV-2E. LV Configuration: Thor DSV-2E 156. FAILURE: At 86 seconds after launch a booster failure occurred and the missile began tumbling.. Failed Stage: 1.
  • BLUEGILL DOUBLE PRIME Nuclear test - . Nation: USA. Agency: USAF. Apogee: 10 km (6 mi). The third attempt to launch a nuclear warhead using a Thor IRBM. At 86 seconds after launch a booster failure occurred and the missile began tumbling. Range safety destroyed the errant booster at 156 seconds after launch. Some radioactive fallout from the warhead was detected on Johnston Atoll.

1962 October 16 - . 15:06 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.31GI.
  • Langmir Probe / CWPE Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 166 km (103 mi).

1963 October 16 - . 16:30 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 619. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2P-221.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1964 October 16 - . LV Family: DF-2. Launch Vehicle: DF-2A.
  • First Chinese atomic bomb tested. - . Nation: China. Program: Long March. Summary: The warhead had a yield of 20 kilotons..

1964 October 16 - . Launch Site: Barking Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Terrier Tomahawk. LV Configuration: Terrier Tomahawk Sandia 152-70. FAILURE: Failure.
  • Terihawk-12 Aeronomy mission - . Nation: USA. Agency: Sandia. Apogee: 0 km ( mi).

1965 October 16 - . 08:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57. LV Configuration: Voskhod 11A57 U15001-04.
  • Cosmos 92 - . Payload: Bion precursor. Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4. Duration: 8.00 days. Decay Date: 1965-10-24 . USAF Sat Cat: 1626 . COSPAR: 1965-083A. Apogee: 331 km (205 mi). Perigee: 204 km (126 mi). Inclination: 64.9000 deg. Period: 89.90 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; also carried weather and biological experiments..

1967 October 16 - .
  • Continued problems with Soyuz landing system tests. - . Nation: USSR. Related Persons: Mishin; Tkachev. Program: Lunar L1; Soyuz. Spacecraft: Soyuz 7K-OK; Soyuz 7K-L1. A further test of the Soyuz landing system went all right, if you don't consider the fact that the 'Tor' altimeter triggered the braking system 3.3 seconds early. One certainly couldn't say, as a result of only these two successful tests, that the system was reliable. The system uses a gamma altimeter, with redundant verification using pulses from HF and UHF antennae. The system has been approved for unmanned flights, but needs additional tests before it can be certified for manned flights. Kholdokov wants the VVS to take over not just trials, but all further development of the landing system, since Mishin and Tkachev are unable to deliver a reliable product. But such a decision can only be taken jointly by the VVS and RVSN.

1967 October 16 - . 08:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 182 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4. Duration: 8.00 days. Decay Date: 1967-10-24 . USAF Sat Cat: 2995 . COSPAR: 1967-098A. Apogee: 374 km (232 mi). Perigee: 197 km (122 mi). Inclination: 64.9000 deg. Period: 90.20 min. Summary: High resolution photo reconnaissance satellite; returned film capsule.

1968 October 16 - . LV Family: Saturn I; Saturn V.
  • Saturn IB program placed in a standby status - . Nation: USA. Related Persons: Phillips, Samuel. Program: Apollo. Flight: Apollo 8. Apollo Program Director Samuel C. Phillips ordered that the Saturn IB program be placed in a standby status pending any future requirements for Apollo or the Apollo Applications program. Phillips' action signaled the shift in Apollo to the Saturn V vehicle, effective with AS-503.

1968 October 16 - . 00:11 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.69UA.
  • Composition Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 340 km (210 mi).

1968 October 16 - . 00:12 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.252GM.
  • Grenades Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 123 km (76 mi).

1968 October 16 - . 08:02 GMT - . 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: 171 km (106 mi).

1968 October 16 - . 23:15 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.248CS.
  • Solar mission - . Nation: USA. Agency: NASA. Apogee: 155 km (96 mi).

1969 October 16 - .
  • Landing of Soyuz 6 - further attempts to dock Soyuz 7 and 8 - . Return Crew: Kubasov; Shonin. Nation: USSR. Related Persons: Shatalov; Filipchenko; Gorbatko; Volkov; Yeliseyev; Kubasov; Shonin. Program: Soyuz. Flight: Soyuz 6; Soyuz 7; Soyuz 8. Spacecraft: Soyuz 7K-OK. 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.

1969 October 16 - . 10:30 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.256GG.
  • Zeta Ori study Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 205 km (127 mi).

1970 October 16 - .
  • Mishin seems to have lost his fight for a water landing on L3 missions. - . Nation: USSR. Related Persons: Mishin; Shatalov; Grechko, Andrei. Program: Lunar L3. Spacecraft: Soyuz 7K-LOK. All will have to be on dry land. 500 million roubles would have been necessary to fund the sea forces, and the risk to the crews would have been greater. Kamanin sees the whole bogus controversy as a diversionary tactic of Mishin's to take attention away from the fact that the L3 spacecraft is in fact nonexistent - as is its N1 rocket. An additional 300 million roubles are needed to achieve a 'flying' N1. A completely new solution to the lunar landing problem needs to be worked out. Shatalov worked today with Grechko to lay out the program for French President Pompidou's visit to the Baikonur cosmodrome. Pompidou wants to see two live rocket launches, and Shatalov will show him the Soyuz spacecraft.

1970 October 16 - . 00:30 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 3 AC. LV Configuration: Skylark 3 AC S53. FAILURE: Failure.
  • ESRO S53 Solar x-ray mission - . Nation: UK. Agency: BAC; ESRO. Apogee: 209 km (129 mi).

1970 October 16 - . 14:59 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53717-04.
  • Cosmos 372 - . Mass: 750 kg (1,650 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-2M. USAF Sat Cat: 4588 . COSPAR: 1970-086A. Apogee: 787 km (489 mi). Perigee: 767 km (476 mi). Inclination: 74.1000 deg. Period: 100.40 min.

1971 October 16 - . Launch Site: Kourou. Launch Complex: Kourou ALFS. LV Family: Stromboli. Launch Vehicle: Eridan. LV Configuration: Eridan E007 (FU-202).
  • ATLAS / CM16 / Gemini Ultraviolet astronomy mission - . Nation: France. Agency: CNES. Apogee: 205 km (127 mi).

1971 October 16 - . 02:31 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 CRL A03.910-1.
  • Infrared Airglow Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 215 km (133 mi).

1972 October 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF25. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • OT GT17GB operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1973 October 16 - . 12:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 600 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4M. Duration: 7.00 days. Decay Date: 1973-10-23 . USAF Sat Cat: 6873 . COSPAR: 1973-074A. Apogee: 340 km (210 mi). Perigee: 205 km (127 mi). Inclination: 72.8000 deg. Period: 90.00 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1973 October 16 - . 14:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC133/1. LV Family: Kosmos 2. Launch Vehicle: Kosmos 11K63.
  • Cosmos 601 - . Payload: DS-P1-Yu s/n 60. Mass: 400 kg (880 lb). Nation: USSR. Agency: MO. Program: DS. Class: Military. Type: Military target satellite. Spacecraft: DS-P1-Yu. Completed Operations Date: 1974-08-15 . Decay Date: 1974-08-15 . USAF Sat Cat: 6875 . COSPAR: 1973-075A. Apogee: 1,135 km (705 mi). Perigee: 195 km (121 mi). Inclination: 81.8000 deg. Period: 98.00 min. Summary: Development of systems for air defence and the control of outer space..

1973 October 16 - . 19:41 GMT - . Launch Site: Andoya. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P141A.
  • High Latitude / Particles Aurora mission - . Nation: UK. Agency: SRC. Apogee: 148 km (91 mi).

1973 October 16 - . 19:43 GMT - . Launch Site: Andoya. LV Family: Skylark. Launch Vehicle: Skylark 6. LV Configuration: Skylark 6 SL1121.
  • UK High Latitude Rocket Ionosphere / aurora mission - . Nation: UK. Agency: BAC. Apogee: 267 km (165 mi).

1974 October 16 - . 02:14 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: 150 km (90 mi).

1975 October 16 - . 02:10 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Apogee: 165 km (102 mi).

1975 October 16 - . 04:04 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/D. LV Configuration: Proton-K/D 287-02. FAILURE: Block D stage failed.. Failed Stage: 4.
  • Ye-8-5M s/n 412 - Block D stage failed. - . Payload: Ye-8-5M s/n 412. Mass: 5,300 kg (11,600 lb). Nation: USSR. Agency: RVSN. Program: Luna. Class: Moon. Type: Lunar probe. Spacecraft: Luna Ye-8-5. Decay Date: 1975-10-16 . COSPAR: F751016A. Summary: Attempted robotic lunar soil return mission. Block D stage failed..

1975 October 16 - . 16:30 GMT - . Launch Site: White Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.000-1.
  • DCST test - . Nation: USA. Agency: USAF CRL. Apogee: 263 km (163 mi).

1975 October 16 - . 22:40 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Delta. Launch Vehicle: Delta 2914. LV Configuration: Delta 2914 597/D116.
  • GOES 1 - . Payload: GOES A. Mass: 295 kg (650 lb). Nation: USA. Agency: NOAA. Class: Earth. Type: Weather satellite. Spacecraft: GOES. Completed Operations Date: 1985-01-01 . USAF Sat Cat: 8366 . COSPAR: 1975-100A. Apogee: 35,811 km (22,251 mi). Perigee: 35,787 km (22,236 mi). Inclination: 14.8000 deg. Period: 1,436.70 min. Geostationary Operational Environmental Satellite. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). Positioned in geosynchronous orbit over the Atlantic Ocean at 55 deg W in 1975-1976; over the Pacific Ocean 135 deg W in 1976-1978; over the Atlantic Ocean 10 deg W in 1978; over the Indian Ocean 58 deg E in 1978-1979; over the Pacific Ocean 135 deg W in 1979-1980; over the Atlantic Ocean 93 deg W in 1980; over the Pacific Ocean 130 deg W in 1980-1985 As of 3 September 2001 located at 81.97 deg W drifting at 0.051 deg E per day. As of 2007 Mar 9 located at 81.95W drifting at 0.055W degrees per day.

1976 October 16 - . 08:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: PRILIV. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 61 km (37 mi).

1976 October 16 - .
  • Landing of Soyuz 23 - . Return Crew: Rozhdestvensky; Zudov. Nation: USSR. Related Persons: Rozhdestvensky; Zudov. Program: Almaz. Flight: Soyuz 23. The capsule landed at 17:46 GMT in Lake Tengiz in -20 deg C conditions in a snowstorm. The wet parachute filled and dragged the capsule below the surface, cooling the capsule. Heating systems had to be turned off in the capsule to conserve battery power. Amphibious vehicles attempted to recover the spacecraft but could not reach it. Finally swimmers managed to attach a cable to a helicopter. The capsule was dragged for kilometres across the icy sea. Only in the morning was the crew able to emerge from the capsule. The recovery crews were surprised they were still alive.

1977 October 16 - . 22:23 GMT - . Launch Site: Andoya. Launch Vehicle: Fulmar. LV Configuration: Fulmar F3.
  • Wind / T Atmospheric mission - . Nation: UK. Agency: SRC. Apogee: 247 km (153 mi).

1977 October 16 - . 22:33 GMT - . Launch Site: Andoya. LV Family: Petrel. Launch Vehicle: Petrel 2. LV Configuration: Petrel 2 P207A.
  • Sodium release Atmospheric mission - . Nation: UK. Agency: SRC. Apogee: 207 km (128 mi).

1978 October 16 - . 21:13 GMT - . Launch Site: Barking Sands. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 59 km (36 mi).

1979 October 16 - . 12:17 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47172-410.
  • Cosmos 1141 - . Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 11585 . COSPAR: 1979-090A. Apogee: 998 km (620 mi). Perigee: 954 km (592 mi). Inclination: 83.0000 deg. Period: 104.60 min. Summary: Military navigation satellite..

1980 October 16 - . 12:20 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1216 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-6U. Duration: 14.00 days. Decay Date: 1980-10-30 . USAF Sat Cat: 12019 . COSPAR: 1980-084A. Apogee: 367 km (228 mi). Perigee: 189 km (117 mi). Inclination: 72.9000 deg. Period: 90.10 min. Summary: Photo surveillance; returned film capsule..

1981 October 16 - . Launch Site: White Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.1027GU.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).

1983 October 16 - .
  • Venera 16, Venus Orbit Insertion - . Nation: USSR. Spacecraft: Venera 4V-2.

1985 October 16 - . 09:25 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1696 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 14.00 days. Decay Date: 1985-10-30 . USAF Sat Cat: 16169 . COSPAR: 1985-095A. Apogee: 270 km (160 mi). Perigee: 205 km (127 mi). Inclination: 70.4000 deg. Period: 89.30 min. Summary: Military cartographic satellite; returned film capsule; maneuverable..

1986 October 16 - . 15:14 GMT - . Launch Site: Ascension. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 67 km (41 mi).

1987 October 16 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 654. Launch Vehicle: Poseidon.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1987 October 16 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 654. Launch Vehicle: Poseidon.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1987 October 16 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 654. Launch Vehicle: Poseidon.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1987 October 16 - . 16:17 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 654. Launch Vehicle: Poseidon.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1989 October 16 - . 14:07 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 82 km (50 mi).

1990 October 16 - . 19:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2102 - . Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 57.00 days. Decay Date: 1990-12-12 . USAF Sat Cat: 20909 . COSPAR: 1990-092A. Apogee: 340 km (210 mi). Perigee: 184 km (114 mi). Inclination: 62.9000 deg. Period: 89.80 min. Summary: High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..

1991 October 16 - . 14:00 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 72 km (44 mi).

1992 October 16 - . Launch Site: Wake Island. Launch Vehicle: Castor-Orbus. LV Configuration: Castor-Orbus-1 SPFE 6. FAILURE: Failure.
  • Re-entry Vehicle test - . Nation: USA. Agency: OSC. Apogee: 500 km (310 mi).

1996 October 16 - . 10:41 GMT - . Launch Site: Wallops Island. LV Family: Super Chief. Launch Vehicle: LCLV. LV Configuration: LCLV Red Tigress 3.
  • Target mission - . Nation: USA. Agency: BMDO. Apogee: 400 km (240 mi).

1996 October 16 - . 16:02 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 36.154NP.
  • DARTFire 2 Microgravity mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

1997 October 16 - . 19:00 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.129DS.
  • EIT-CALROC Solar mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 350 km (210 mi).

1997 October 16 - . 19:13 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3B. LV Configuration: Chang Zheng 3B CZ3B-3 (48).
  • Apstar 2R - . Nation: China. Agency: APT. Manufacturer: Palo Alto. Program: Apstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 25010 . COSPAR: 1997-062A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Geosynchronous. Stationed over 76.5E Positioned in geosynchronous orbit at 76 deg E in 1997-1999 As of 5 September 2001 located at 76.48 deg E drifting at 0.001 deg W per day. As of 2007 Mar 11 located at 76.46E drifting at 0.002W degrees per day..

2000 October 16 - . 14:15 GMT - .
  • EVA STS-92-2 - . Crew: Wisoff; Lopez-Alegria. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.30 days. Nation: USA. Related Persons: Wisoff; Lopez-Alegria. Program: ISS. Class: Manned. Type: Manned space station. Flight: STS-92. Spacecraft: International Space Station. Wakata aboard the shuttle used the RMS arm to unberth the PMA-3 docking unit from the SLP pallet at 16:14 GMT, and docked it to Unity at 17:40 GMT. Wisoff and Lopez-Alegria first unbolted PMA-3 from the SLP and then guided Wakata through the delicate alignment process as PMA-3 was removed from the bay and attached to the Station.

2000 October 16 - . 21:27 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U K15000-085.
  • Progress M-43 - . Payload: Progress M s/n 243. Mass: 6,860 kg (15,120 lb). Nation: Russia. Agency: RAKA. Manufacturer: Korolev. Program: Mir. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Progress M. Duration: 101.00 days. Decay Date: 2001-01-29 . USAF Sat Cat: 26570 . COSPAR: 2000-064A. Apogee: 228 km (141 mi). Perigee: 186 km (115 mi). Inclination: 51.6000 deg. Period: 88.64 min. Mir Servicing flight. Launch delayed from October 15. Progress docked with Mir, primarily to raise its orbit and preserve the option of a MirCorp-financed flight in 2001. However the funding never came through and the decision was taken to deorbit Mir. Progress M-43 undocked at 0519 GMT on January 25 from the +X Kvant port to clear it for Progress M1-5 (which would deorbit the Mir station). On January 29 Progress M-43 was in a 271 x 280 km x 51.6 deg orbit.

2002 October 16 - . Launch Site: Mojave. Launch Vehicle: Tier One.
  • White Knight Flight 8 - . Nation: USA. Related Persons: Binnie; Melvill. Program: X-Prize. Spacecraft: SpaceShipOne. Flight Time: 1.6 hours Pilot: Melvill Copilot: Binnie. Objectives: Envelope expansion above 50,000 feet and 0.55M. Avionics software upgrade. Practice SpaceShipOne glide approaches Results: Climbed to 53,000 feet and 0.53M in Military power. Cleared the full required envelope needed for SpaceShipOne launch operations. Flying qualities at highest altitude are satisfactory and will not require dampers. Window fogging not an issue until the cabin was depressurized at 10,000 feet.

2004 October 16 - .
2005 October 16 - .
2005 October 16 - . 20:33 GMT - .
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