Encyclopedia Astronautica
November 09


November 09 Chronology


1898 November 9 - .
  • Birth of Hugo Broetler - . Nation: Germany; Russia. Summary: German welding engineer in WW2, member of the Rocket Team in the Soviet Union, worked on rocket engine development in Glushko's design bureau from 1947 to 1952. Worked in Oxygen Plant; Shop 55..

1902 November 9 - .
  • Birth of Mitrofan Ivanovich Nedelin - . Nation: Russia. Summary: Russian officer. Deputy Minister of Defence 1955-1959. First Commander-in-Chief of the Strategic Missile Forces 1959-1964. Died in the Nedelin catastrophe..

1906 November 9 - .
  • Birth of Arthur Louis Hugo Rudolph - . Nation: Germany; USA. Summary: German-American rocket engineer, with Valier in 1931, von Braun from 1934. Planned V-2 production. Program manager for Redstone, Pershing, and the Saturn V. Retired 1970, but named as a war criminal, returned to Germany in 1984..

1908 November 9 - .
1918 November 9 - .
  • Birth of Spiro T Agnew - . Nation: USA. Summary: American politician. Vice President of the United States, 1968-1973..

1921 November 9 - .
  • Birth of Thomas O Paine - . Nation: USA. Summary: American engineer, at General Electric, then NASA Administrator 1968-1970. His ambitious post-Apollo programs were not received well by the Nixon administration..

1941 November 9 - .
  • Von Braun promoted to SS Obersturmfuehrer. - . Nation: Germany. Related Persons: von Braun.

1942 November 9 - .
  • Von Braun promoted to SS Hauptsturmfuehrer. - . Nation: Germany. Related Persons: von Braun.

1943 November 9 - . Launch Site: Peenemuende. Launch Complex: Peenemuende P7. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-043.
1944 November 9 - . Launch Site: Heidekraut. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 19520.
  • V-2 Ma285 236 M1 - . Nation: Germany. Summary: Planned range 250 km. Impact 6.2 km to the right of the planned trajectory. Circular error 9.4 km from aim point..

1948 November 9 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 29R.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1950 November 9 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Hermes. Launch Vehicle: Hermes B-1. LV Configuration: Hermes B-1 B-1 No. 2A.
  • Hermes II test - . Nation: USA. Agency: USA. Apogee: 150 km (90 mi).

1950 November 9 - . Launch Site: Wallops Island. LV Family: HVAR. Launch Vehicle: HVAR FFAR.
  • F25 Drag Model test flight - . Nation: USA. Agency: NASA. Apogee: 5.00 km (3.10 mi).

1951 November 9 - . Launch Site: Edwards.
  • XS-1 No. 3 destroyed in ground explosion. - . Crew: Cannon. Payload: XS-1 # 3 flight 1. Nation: USA. Related Persons: Cannon. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: Planned captive flight with B-50 for propellant jettison test. XS-1 (No. 3) rocket research airplane and its B-29 "mother" airplane were destroyed on the ground by postflight explosion and fire. Pilot Cannon was injured..

1952 November 9 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bechar. LV Family: Veronique. Launch Vehicle: Veronique. LV Configuration: Veronique N5. FAILURE: Failure.
  • Test mission - . Nation: France. Agency: LRBA. Apogee: 1.00 km (0.60 mi).

1954 November 9 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 3331T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1956 November 9 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador. LV Configuration: Matador GM-54-127.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1957 November 9 - . 16:54 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: V-2. Launch Vehicle: R-1. LV Configuration: A-1.
  • Ionosphere / aeronomy mission - . Nation: USSR. Agency: MVS. Apogee: 330 km (200 mi).

1959 November 9 - . LV Family: Titan. Launch Vehicle: Titan 1.
  • Contractor selection for Dynasoar and Titan I announced. - . Nation: USA. Class: Manned. Type: Manned spaceplane. Spacecraft: Dynasoar. Boeing and Martin selected by USAF to develop Dynasoar and Titan I launch vehicle. The compromise project reformulation a week earlier led to this announcement by the Secretary of the Air Force. Boeing was the winner of the DynaSoar design competition on 9 November 1959 - but for the glider and total system only. Martin was selected as an associate contractor for booster development. Dynasoar received the designation WS-620A on 17 November 1959

1960 November 9 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador. LV Configuration: Matador GM-56-1938.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1961 November 9 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC29A. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2X-14 (A2G-1).
  • Test mission - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1961 November 9 - . 17:57 GMT - . Launch Site: Mud Lake DZ. Launch Pad: 37.9 N x 117.1 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 2-21-37. FAILURE: Right windshield cracks..
  • X-15A Mach 6, Aero, Stab test - . Nation: USA. Agency: NASA; USAF. Apogee: 31 km (19 mi). Summary: Design speed achieved. Outer right windshield shattered. Maximum Speed - 6586 kph. Maximum Altitude - 30950 m..

1962 November 9 - .
  • Plans for additional Vostoks quashed - . Nation: USSR. Program: Vostok. Flight: Vostok 7; Vostok 8; Vostok 9; Vostok 10; Vostok 11; Vostok 12; Vostok 13. Kamanin prepared recommendations for General Staff discussions on future Vostok military flights. His plan involved construction of ten additional spacecraft including new versions to test military equipment for reconnaisance, interception, and combat objectives. Flights would begin in 1963: manned flights of ten days duration; flights with biological payloads of 30 days duration; flights with biological payloads in high orbits to test the effects of Van Allen radiation belt exposure; flights that would conduct a range of technology experiments, including manual landing; landing with the cosmonaut within the capsule; depressurisation of the capsule to vacuum test equipment and suits for future spacewalks; etc). The plan was killed by his superiors.

1962 November 9 - .
  • Raytheon contracted for the Apollo spacecraft guidance computer - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Guidance. Summary: The Manned Spacecraft Center (MSC) and the Raytheon Company came to terms on the definitive contract for the Apollo spacecraft guidance computer..

1962 November 9 - . 03:12 GMT - . Launch Site: Point Mugu. LV Family: Nike Zeus. Launch Vehicle: Nike Zeus. LV Configuration: Nike Zeus-3.
  • PM-16? sim target - . Nation: USA. Agency: USA. Apogee: 200 km (120 mi).

1962 November 9 - . 18:23 GMT - . Launch Site: Mud Lake DZ. Launch Pad: 37.9 N x 117.1 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 2-31-52. FAILURE: Engine failure. Crash landing on Mud Lake..
  • X-15A VO Stab, Bound.Layer test - . Nation: USA. Agency: NASA; USAF. Apogee: 16 km (9 mi). Summary: Engine only produced 35% power. Emergency landing at Mud Lake. Aircraft seriously damaged when gear failed. McKay injured. Maximum Speed - 1640 kph. Maximum Altitude - 16450 m..

1963 November 9 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-C. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-27.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 November 9 - . 20:27 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Delta. Launch Vehicle: Thor Agena D SLV-2. LV Configuration: Thor SLV-2 Agena D 400 / Agena D 1171. FAILURE: Failure. Failed Stage: U.
  • KH-4 9060 - . Payload: KH-4 s/n 9060. Mass: 1,150 kg (2,530 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-4. Decay Date: 1963-11-09 . COSPAR: F631109A. Summary: KH-4. Mission failed..
  • SRV 632 - . Nation: USA. Agency: USAF. Spacecraft: KH-4. COSPAR: F631109B.

1964 November 9 - . Launch Site: Barking Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-67.
  • Ballistic HRT Aeronomy mission - . Nation: USA. Agency: Sandia. Apogee: 289 km (179 mi).

1964 November 9 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 661.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1964 November 9 - . 12:54 GMT - . Launch Site: Thumba. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.204IA.
  • ISRO 10.05 / TERLS-13? Aeronomy sodium release mission - . Nation: USA. Agency: NASA. Apogee: 192 km (119 mi).

1965 November 9 - . Launch Site: Eglin. LV Family: Honest John. Launch Vehicle: HJ Nike Hydac.
  • Aeronomy mission? [113 kg] - . Nation: USA. Agency: USAF. Apogee: 521 km (323 mi).

1965 November 9 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2009.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 November 9 - . 09:58 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Vehicle: HAD. LV Configuration: HAD 179.
  • Aeronomy mission - . Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi).

1965 November 9 - . 18:40 GMT - . Launch Site: Fort Churchill. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.168UA.
  • UM Pitot 18 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 144 km (89 mi).

1965 November 9 - . 19:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 CRL AF3.523.
  • Extreme ultraviolet Mon Solar extreme ultraviolet mission - . Nation: USA. Agency: USAF. Apogee: 238 km (147 mi).

1965 November 9 - . 19:16 GMT - . Launch Site: Fort Churchill. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.03GA.
  • Thermosphere Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 328 km (203 mi).

1966 November 9 - .
1967 November 9 - . 12:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Saturn V. Launch Vehicle: Saturn V. LV Configuration: Saturn V SA-501.
  • Apollo 4 - . Payload: Apollo CSM 017 / LTA-10R / S-IVB-501. Mass: 36,656 kg (80,812 lb). Nation: USA. Agency: NASA Houston. Program: Apollo. Class: Moon. Type: Manned lunar spacecraft. Spacecraft: Apollo CSM; CSM Parachute. Duration: 2.35 days. Decay Date: 1967-11-09 . USAF Sat Cat: 3032 . COSPAR: 1967-113A. Apogee: 371 km (230 mi). Perigee: 370 km (220 mi). Inclination: 32.7000 deg. Period: 91.90 min. Apollo 4 (AS-501) was launched in the first all-up test of the Saturn V launch vehicle and also in a test of the CM heatshield. The Saturn V, used for the first time, carried a lunar module test article (LTA-10R) and a Block I command and service module (CSM 017) into orbit from KSC Launch Complex 39, Pad A, lifting off at 7:00:01 a.m. EST - one second later than planned. The launch was also the first use of Complex 39. The spacecraft landed 8 hours 37 minutes later in the primary recovery area in the Pacific Ocean, near Hawaii, about 14 kilometers from the planned point (30.06 N 172.32 W). CM, apex heatshield, and one main parachute were recovered by the carrier U.S.S. Bennington

    Main objectives of the mission were to demonstrate the structural and thermal integrity of the space vehicle and to verify adequacy of the Block II heatshield design for entry at lunar return conditions. These objectives were accomplished.

    The S-IC stage cutoff occurred 2 minutes 30 seconds into the flight at an altitude of about 63 kilometers. The S-II stage ignition occurred at 2 minutes 32 seconds and the burn lasted 6 minutes 7 seconds, followed by the S-IVB stage ignition and burn of 2 minutes 25 seconds. This series of launch vehicle operations placed the S-IVB and spacecraft combination in an earth parking orbit with an apogee of about 187 kilometers and a perigee of 182 kilometers. After two orbits, which required about three hours, the S-IVB stage was reignited to place the spacecraft in a simulated lunar trajectory. This burn lasted five minutes. Some 10 minutes after completion of the S-IVB burn, the spacecraft and S-IVB stage were separated, and less than 2 minutes later the service propulsion subsystem was fired to raise the apogee. The spacecraft was placed in an attitude with the thickest side of the CM heatshield away from the solar vector. During this four-and-one-half-hour cold-soak period, the spacecraft coasted to its highest apogee - 18,256.3 kilometers. A 70 mm still camera photographed the earth's surface every 10.6 seconds, taking 715 good-quality, high-resolution pictures.

    About 8 hours 11 minutes after liftoff the service propulsion system was again ignited to increase the spacecraft inertial velocity and to simulate entry from a translunar mission. This burn lasted four and one half minutes. The planned entry velocity was 10.61 kilometers per second, while the actual velocity achieved was 10.70.

    Recovery time of 2 hours 28 minutes was longer than anticipated, with the cause listed as sea conditions - 2.4-meter swells.


1968 November 9 - .
  • Zond 6 State Commission - . Nation: USSR. Program: Lunar L1. Flight: Soyuz 7K-L1 mission 1. Spacecraft: Soyuz 7K-L1. Summary: The State Commission for the flight of L1 s/n 12 meets at Tyuratam. Launch is set for 10 November. Kamanin notes that the Americans plan to fly Apollo 8 to the moon at great risk in December, but the Russians will not undertake such risk..

1968 November 9 - . Launch Site: Biscarosse. Launch Complex: Biscarosse BLB. LV Family: SSBS. Launch Vehicle: SSBS S01.
  • S01C-2 test - . Nation: France. Agency: DMA. Apogee: 500 km (310 mi).

1968 November 9 - . 08:55 GMT - . Launch Site: Fort Churchill. LV Family: Javelin. Launch Vehicle: Javelin. LV Configuration: Javelin CRL AB19.287.
  • P / F Plasma mission - . Nation: USA. Agency: USAF. Apogee: 592 km (367 mi).

1969 November 9 - . 16:47 GMT - . Launch Site: Atlantic Ocean. Launch Pad: 45.0 N x 46.0 W. Launch Platform: ZUB. LV Family: MR-12. Launch Vehicle: MR-12.
  • Ionosphere mission - . Nation: USSR. Agency: AN. Apogee: 162 km (100 mi).

1970 November 9 - .
  • Cosmonauts have perfect flight safety record since Gagarin's crash. - . Nation: USSR. Related Persons: Shatalov; Yeliseyev. Summary: The cosmonaut's Seregin Regiment has now flown 4500 hours without an accident. The safety record for the VVS was 18,000 hours between crashes in 1969, 22,000 in 1970 so far..

1970 November 9 - . 06:00 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA3A. LV Family: Scout. Launch Vehicle: Scout B. LV Configuration: Scout B S174C.
  • OFO 1 - . Payload: OFO 1 / RM 1. Mass: 133 kg (293 lb). Nation: USA. Agency: NASA Ames. Class: Biology. Type: Biology satellite. Spacecraft: OFO. Decay Date: 1971-05-09 . USAF Sat Cat: 4690 . COSPAR: 1970-094A. Apogee: 518 km (321 mi). Perigee: 304 km (188 mi). Inclination: 37.4000 deg. Period: 92.60 min. Orbiting Frog Otolith. The satellite carrying the OFO-A experiment remained in orbit for almost seven days. Recovery of the spacecraft was not planned. The payload was the Frog Otolith Experiment Package (FOEP). The objective of the experiment was to investigate the effect of microgravity on the otolith, a sensory organ that responds to changes in an animal's orientation within the Earth's gravitational field. Two bullfrogs (Rana catesbeiana) were used as experimental subjects in the flight experiment. Additional Details: OFO 1.
  • RM-1; RMS - . Payload: RM/FW4S. Mass: 46 kg (101 lb). Nation: USA. Agency: NASA Houston. Class: Earth. Type: Micrometeoroid satellite. Spacecraft: RM. Decay Date: 1971-02-07 . USAF Sat Cat: 4692 . COSPAR: 1970-094B. Apogee: 526 km (326 mi). Perigee: 303 km (188 mi). Inclination: 37.4000 deg. Period: 92.70 min. Summary: Radiation Meteoroid. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .

1971 November 9 - . 19:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 CRL A03.002-4.
  • XUV Solar ultraviolet / solar extreme ultraviolet mission - . Nation: USA. Agency: AFCRL. Apogee: 215 km (133 mi).

1971 November 9 - . 19:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 CRL A03.002-3.
  • XUV Solar ultraviolet / solar extreme ultraviolet mission - . Nation: USA. Agency: AFCRL. Apogee: 219 km (136 mi).

1972 November 9 - .
  • M2 Flight 38 - . Crew: Powell. Payload: M2-F3 flight 22. Nation: USA. Related Persons: Powell. Program: NASA Lifting Body. Class: Manned. Type: Manned spaceplane. Spacecraft: M2-F3. Summary: Maximum Speed - 961 kph. Maximum Altitude - 14260 m. Flight Time - 364 sec..

1972 November 9 - . 03:23 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC10W. LV Family: Delta. Launch Vehicle: Thor Burner 2A. LV Configuration: Thor Burner 2A 294.
  • DMSP-Block-5B F3 - . Payload: DMSP 6530 / OPS 7323. Mass: 195 kg (429 lb). Nation: USA. Agency: USAF. Program: DMSP. Class: Earth. Type: Weather satellite. Spacecraft: DMSP Block 5B. USAF Sat Cat: 6275 . COSPAR: 1972-089A. Apogee: 841 km (522 mi). Perigee: 785 km (487 mi). Inclination: 98.6000 deg. Period: 101.10 min. Summary: Defense Meteorological Satellite Program..

1973 November 9 - . 17:15 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA8. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.106UG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 169 km (105 mi).

1973 November 9 - . 18:00 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA8. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.105UG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 175 km (108 mi).

1976 November 9 - . 12:32 GMT - . Launch Site: Woomera. LV Family: Black Brant. Launch Vehicle: Black Brant 5B. LV Configuration: Black Brant VB APD-VB-42.
  • Cosmic rays X-ray astronomy mission - . Nation: Canada. Agency: NRCC. Apogee: 215 km (133 mi).

1977 November 9 - . 15:40 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 78 km (48 mi).

1978 November 9 - . 04:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 83 km (51 mi).

1979 November 9 - . 20:25 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 84 km (52 mi).

1981 November 9 - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Honest John. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.21UL.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1982 November 9 - . 17:45 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Black Brant. Launch Vehicle: Black Brant 5B. LV Configuration: Black Brant VB NASA 21.64GS.
  • Extreme ultraviolet line profiles Solar mission - . Nation: USA. Agency: NASA. Apogee: 233 km (144 mi).

1983 November 9 - . 05:15 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk GL A08.708-2.
  • IMS Release (SF6) Plasma release mission - . Nation: USA. Agency: USAF. Apogee: 348 km (216 mi).

1984 November 9 - . 20:00 GMT - . Launch Site: Eareckson. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 52 km (32 mi).

1985 November 9 - . 08:25 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL.
  • Cosmos 1701 - . Payload: Oko #45. Mass: 1,250 kg (2,750 lb). Nation: USSR. Agency: MOM. Class: Military. Type: Early warning satellite. Spacecraft: Oko. Decay Date: 2001-05-11 . USAF Sat Cat: 16235 . COSPAR: 1985-105A. Apogee: 36,974 km (22,974 mi). Perigee: 3,375 km (2,097 mi). Inclination: 67.2000 deg. Period: 717.70 min. Summary: Replaced Cosmos 1675. Covered Oko constellation plane 8 - 192 degree longitude of ascending node..

1987 November 9 - . Launch Site: Vandenberg.
  • Last launch of a Minuteman II - . Nation: USA. Summary: Last launch of a Minuteman II (first launch from Vandenberg AFB on 18 August 1965)..

1988 November 9 - .
  • Death of Charles Stuart 'Charlie' Ames - . Nation: USA. Related Persons: Ames, Charles. Summary: American engineer, son of an iron works machinist, Project Engineer on the MX-774 and early Atlas programs. He was remembered as rock-solid, smart, practical, able to obtain the best designs by trading off inter-departmental concepts..

1988 November 9 - . 14:07 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 81 km (50 mi).

1989 November 9 - . 15:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 82 km (50 mi).

1990 November 9 - . 17:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 82 km (50 mi).

1994 November 9 - .
  • Mir News 237: Progress-M25 - . Nation: Russia. Program: Mir. Flight: Mir Euromir 94; Mir EO-16; Mir EO-17; Mir LD-4. Summary: The launch of this freighter from Baykonur is on schedule for 11 November 1994 at 0721 UTC. If all goes according to plan Progress-M25 will dock to the Mir-complex in the morning of 13 November 1994.

    Chris v.d. Berg, NL-9165-A-UK3202.


1995 November 9 - . 02:15 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P. LV Configuration: MT-135P-R942.
  • Meteorological mission - . Nation: Japan. Agency: JMA. Apogee: 60 km (37 mi).

1996 November 9 - . 08:50 GMT - . Launch Site: Plesetsk. LV Family: Topol. Launch Vehicle: Topol. LV Configuration: Topol 52.
  • Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1997 November 9 - . 01:34 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Delta. Launch Vehicle: Delta 7920-XC. LV Configuration: Delta 7920-10C D250.
  • Iridium 43 - . Payload: Iridium s/n SV043. Mass: 689 kg (1,518 lb). Nation: USA. Agency: Iridium. Manufacturer: Lockheed; Motorola. Program: Iridium. Class: Communications. Type: Civilian communications satellite. Spacecraft: LM 700. USAF Sat Cat: 25039 . COSPAR: 1997-069A. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.3900 deg. Period: 100.40 min. Summary: Plane 6. Ascending node 325.8 degrees..
  • Iridium 41 - . Payload: Iridium s/n SV041. Mass: 689 kg (1,518 lb). Nation: USA. Agency: Iridium. Manufacturer: Lockheed; Motorola. Program: Iridium. Class: Communications. Type: Civilian communications satellite. Spacecraft: LM 700. USAF Sat Cat: 25040 . COSPAR: 1997-069B. Apogee: 780 km (480 mi). Perigee: 776 km (482 mi). Inclination: 86.4000 deg. Period: 100.40 min. Summary: Plane 6. Ascending node 325.8 degrees..
  • Iridium 38 - . Payload: Iridium s/n SV038. Mass: 689 kg (1,518 lb). Nation: USA. Agency: Iridium. Manufacturer: Lockheed; Motorola. Program: Iridium. Class: Communications. Type: Civilian communications satellite. Spacecraft: LM 700. USAF Sat Cat: 25043 . COSPAR: 1997-069E. Apogee: 780 km (480 mi). Perigee: 776 km (482 mi). Inclination: 86.4000 deg. Period: 100.40 min. Summary: Plane 6. Ascending node 325.6 degrees..
  • Iridium 40 - . Payload: Iridium s/n SV040. Mass: 689 kg (1,518 lb). Nation: USA. Agency: Iridium. Manufacturer: Lockheed; Motorola. Program: Iridium. Class: Communications. Type: Civilian communications satellite. Spacecraft: LM 700. USAF Sat Cat: 25041 . COSPAR: 1997-069C. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.3900 deg. Period: 100.40 min. Summary: Plane 6. Ascending node 325.8 degrees..
  • Iridium 39 - . Payload: Iridium s/n SV039. Mass: 689 kg (1,518 lb). Nation: USA. Agency: Iridium. Manufacturer: Lockheed; Motorola. Program: Iridium. Class: Communications. Type: Civilian communications satellite. Spacecraft: LM 700. USAF Sat Cat: 25042 . COSPAR: 1997-069D. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.4000 deg. Period: 100.40 min. Summary: Plane 6. Ascending node 325.8 degrees..

2000 November 9 - .
  • ISS Status Report: ISS 00-54 - . Nation: USA. Related Persons: Gidzenko; Shepherd. Program: ISS. Flight: ISS EO-1. Summary: The Expedition One crew today activated the last of its critical life support systems aboard the International Space Station and looked ahead to the launch of a resupply vehicle next week to the new outpost.. Additional Details: ISS Status Report: ISS 00-54.

2001 November 9 - .
  • STARS missile defense target vehicle failure. - . Nation: USA. Summary: A suborbital STARS missile defense target (Polaris with Orbus-1 upper stage) was destroyed during launch from Kodiak. .

2002 November 9 - .
2005 November 9 - .
  • Hayabusa releases target marker. - . Nation: Japan. Summary: Hayabusa released the first of three 10-cm target markers towards the surface of asteroid Itokawa. It missed the surface and floated off into deep space..

2005 November 9 - . 03:33 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz-FG/Fregat Zh15000-010.
  • Venus Express - . Mass: 1,270 kg (2,790 lb). Nation: Europe. Agency: ESA. Class: Venus. Type: Venus probe. Spacecraft: Venus Express. USAF Sat Cat: 28901 . COSPAR: 2005-045A. Launch delayed from October 26. The Soyuz placed the probe and Fregat upper stage into a 30 km x 190 km x 51.6 deg orbit around the earth. At apogee the Fregat stage made a 50 m/s maneuver to circularize the orbit. At the appropriate moment in this parking orbit, the Fregat fired again, then separated from the now Venus-bound probe at 05:11 GMT. Venus Express passed lunar orbit on November 10 at 10:10 GMT and went into a 0.702 AU x 0.993 AU x 0.26 deg inclination solar orbit. It was to brake itself into a 250 km x 326,550 km x 89.7 deg orbit around Venus on 11 April 2006 at 08:40 GMT. Two maneuvers would put in its final 24-hour Venus orbit of 282 x 66,911 km x 90.0 deg on 30 April. This was selected to synchronise the satellite with tracking stations on earth, while the planet slowly revolves below its perigee point over the following several months.

2006 November 9 - . 08:51 GMT - . Launch Site: Biscarosse. LV Family: MSBS. Launch Vehicle: MSBS M51. LV Configuration: MSBS M51 1.
  • M51 test launch - . Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi).

2006 November 9 - . 11:35 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC175/2. Launch Pad: LC175/pad?. LV Family: UR-100N. Launch Vehicle: UR-100NU.
  • Operational missile test - . Nation: Kazakhstan. Agency: RVSN. Apogee: 1,000 km (600 mi).

2007 November 9 - . 09:54 GMT - .
  • EVA ISS EO-16-1 - . Crew: Whitson; Malenchenko. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.29 days. Nation: USA. Related Persons: Whitson; Malenchenko. Program: ISS. Flight: ISS EO-16; ISS EO-16-1. The astronauts conducted exterior work in preparation for the move of the Pressurized Mating Adapter 2 (PMA-2) from the Destiny lab and to the Harmony module. They disconnected and stowed cables, removed a light on one of the stationís transport carts and took the cover off Harmony's Common Berthing Mechanism. They also removed a base-band signal processor for later refurbishment; removed a remote power controller module that was to be replaced; and transferred tools in preparation for upcoming spacewalks.

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