Encyclopedia Astronautica
November 14


November 14 Chronology


1907 November 14 - .
  • Birth of Leonid Ivanovich Sedov - . Nation: Russia. Summary: Russian scientist. Chaired the Commission for Promotion of Interplanetary Flights. Public spokesman for the Soviet space program..

1910 November 14 - .
  • Birth of Harry J Goett - . Nation: USA. Summary: American engineer. At Langley from 1936, headed flight research at Ames 1958-1959, director of Goddard 1959-1965. Headed important 1960 committee that established NASA LV development plans. At Ford Aerospace from 1965..

1914 November 14 - .
1919 November 14 - .
  • Birth of Kerim Aliyevich Kerimov - . Nation: Russia. Summary: Russian officer. First Commander of TsUKOS 1964-1965. Directorate Chief of Ministry of General Machine Building 1965-1974..

1930 November 14 - .
  • Birth of Edward Higgins II 'Ed' White - . Nation: USA. Summary: American test pilot astronaut. Flew on Gemini 4. First American to walk in space. Died in on-pad fire of Apollo 1..

1933 November 14 - .
  • Birth of Fred Wallace Jr 'Pecky' Haise - . Nation: USA. Summary: American pilot astronaut. Flew on Apollo 13. Survived first emergency beyond low earth orbit. Altitude (401,056 km) record..

1934 November 14 - .
  • Birth of Rudolf Alekseyevich Gulyayev - . Nation: Russia. Summary: Russian scientist cosmonaut, 1967-1968. Scientist, Institute of Terrastrial Magnetism & Radiowaves of AN. Cosmonaut training May 1967 - August 1968. Left cosmonaut team for medical reasons. Worked as a research scientist at IZMIRAN..

1935 November 14 - .
  • Birth of Gennadi Aleksandrovich Dolgopolov - . Nation: Russia. Summary: Russian engineer cosmonaut, 1966-1967. Graduated from Moscow Aviation Institute (MAI), 1959 Civilian Engineer, Korolev OKB. Retired due to medical reasons. Worked thereafter at NPO Energia..

1944 November 14 - . Launch Site: Heidekraut. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 19525.
  • V-2 Ma283 241 M8 - . Nation: Germany. Summary: Planned range 250 km. Impact 0.5 km to the right of the planned trajectory. Circular error 0.5 km from aim point..

1947 November 14 - . Launch Site: Wallops Island. LV Family: FFAR. Launch Vehicle: Double FFAR.
  • D-558-II model test flight - . Nation: USA. Agency: NASA. Apogee: 5.00 km (3.10 mi).

1951 November 14 - . Launch Site: White Sands. LV Family: Honest John. Launch Vehicle: Honest John. LV Configuration: Honest John 11.
  • Test mission - . Nation: USA. Apogee: 10 km (6 mi).

1952 November 14 - . Launch Site: Wallops Island. LV Family: HVAR. Launch Vehicle: HVAR FFAR.
  • E31 model test flight - . Nation: USA. Agency: NASA. Apogee: 5.00 km (3.10 mi).

1956 November 14 - .
1956 November 14 - . 02:05 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC6. LV Family: Redstone. Launch Vehicle: Jupiter A. LV Configuration: Jupiter A RS-28. FAILURE: Human error in propellant loading plus programmed fuel depletion cut-off..
  • Jupiter A/Sandia PL - . Nation: USA. Agency: USA. Apogee: 90 km (55 mi). RS-28 was launched at 2105 EST from AMR. The flight was successful. Actual range was 152.4 nm; 9.51 nm over; and 1.5 kilometres left of the intended impact point. The missile carried the LEV-3 rather than the ST-80 guidance system and used fuel depletion cut-off. The primary test objective was to test the Sandia payload. Missed aimpoint by 19,500 m.

1957 November 14 - .
  • UN calls for inspections to insure objects in outer space only for peaceful purposes - . Nation: International. The General Assembly of the United Nations adopted Resolution 1148 (XII), calling, in part, for "the joint study of an inspection system designed to ensure that the sending of objects through outer space shall be exclusively for peaceful and scientific purposes."

1958 November 14 - .
  • Specifications for Mercury issued. - . Nation: USA. Program: Mercury. Spacecraft: Mercury. Summary: Specifications for the manned spacecraft (Specification Number S-6) were issued, and final copies were mailed on November 17, 1958, to 20 firms which had indicated a desire to be considered as bidders..

1958 November 14 - .
  • Twenty firms to bid on Mercury spacecraft. - . Nation: USA. Program: Mercury. Spacecraft: Mercury. Summary: Twenty firms notified the National Aeronautics and Space Administration of their intention to prepare proposals for the development of the manned spacecraft. NASA set the deadline for proposal submission as December 11, 1958..

1958 November 14 - .
  • DX priority requested for Mercury project. - . Nation: USA. Program: Mercury. Summary: The highest national procurement priority rating (DX) was requested for the manned spacecraft project..

1959 November 14 - . 22:38 GMT - . Launch Site: Fort Churchill. LV Family: Aerobee. Launch Vehicle: Aerobee 300. LV Configuration: Aerobee 300 AA10.165C.
  • GRD sphere Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 138 km (85 mi).

1960 November 14 - . LV Family: DF-3. Launch Vehicle: DF-3.
  • DF-3 ICBM development begun. - . Nation: China. Related Persons: Tsien. Program: Long March. Tsien appoints himself head of the DF-3 project - a quantum leap to build a 10,000 km range liquid oxygen/kerosene propellant intercontinental ballistic missile. The objective proves much too ambitious and is eventually cancelled. It is the last missile project Tsien is allowed to manage.

1961 November 14 - . Launch Vehicle: Al Zahar.
  • Egypt first rocket launch. - . Nation: Egypt. Apogee: 10 km (6 mi). United Arab Republic neither confirmed nor denied reports of November 8 that it had successfully launched its first rocket. Dr. Eugen Saenger of the Stuttgart Jet Propulsion Institute in Germany denied any connection with the United Arab Republic program as charged by Israel.

1962 November 14 - . 22:36 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg OSTF2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 13F. FAILURE: Failure. Failed Stage: 1.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 300 km (180 mi).

1963 November 14 - .
  • Cancellation of X-20 program proposed. - . Nation: USA. Spacecraft: Dynasoar; MOL. The Director of Defense for Research and Engineering recommended to the Secretary of Defense cancellation of the X-20 program and initiation of a space station program. Harold Brown believed that Blue Gemini could accommodate significantly greater payload for such missions. He recommended that DynaSoar be cancelled and replaced by a Gemini-serviced space station.

1963 November 14 - .
  • The resolution is issued on final selection of the second cosmonaut group. - . Nation: USSR.

1963 November 14 - . Launch Site: Kwajalein. LV Family: Nike Zeus. Launch Vehicle: Nike Zeus. LV Configuration: Nike Zeus-3.
  • K-24 Titan Intercept - . Nation: USA. Agency: USA. Apogee: 200 km (120 mi).

1963 November 14 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-A1. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I SM-68.
  • Demonstration and shakedown operations launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi).

1963 November 14 - . 19:19 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 1-41-65.
  • X-15A CO/Opt Deg/Systems Test/Technology mission - . Nation: USA. Agency: NASA; USAF. Apogee: 27 km (16 mi). Summary: Maximum Speed - 5287 kph. Maximum Altitude - 27680 m..

1964 November 14 - . 10:23 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.110GG.
  • Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 207 km (128 mi).

1965 November 14 - . Launch Site: Baikonur. Launch Complex: Baikonur PU32. LV Family: Tsiklon. Launch Vehicle: R-36 8K67.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1966 November 14 - .
  • M2 Flight 13 - . Crew: Gentry. Payload: M2-F2 flight 13. Nation: USA. Related Persons: Gentry. Program: NASA Lifting Body. Class: Manned. Type: Manned spaceplane. Spacecraft: M2-F2. Summary: Maximum Speed - 642 kph. Maximum Altitude - 13720 m. Flight Time - 261 sec..

1966 November 14 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 655. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-394.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1966 November 14 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 655. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-512.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1966 November 14 - . 11:28 GMT - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bacchus. Launch Pad: Bacchus?. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C105.
  • FU-167 Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 150 km (90 mi).

1966 November 14 - . 13:03 GMT - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bacchus. Launch Pad: Bacchus?. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C139.
  • FU-167 Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 150 km (90 mi).

1966 November 14 - . 14:52 GMT - .
  • EVA Gemini 12-3 - . Crew: Aldrin. EVA Type: Stand-Up External Vehicular Activity. EVA Duration: 0.0382 days. Nation: USA. Related Persons: Aldrin. Program: Gemini. Class: Manned. Type: Manned spacecraft. Flight: Gemini 12. Spacecraft: Gemini. Summary: Photographed earth limb and stars in ultraviolet..

1966 November 14 - . 20:38 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA6A. LV Family: Europa. Launch Vehicle: Europa. LV Configuration: ELDO A F-5.
  • Active first stage with dummy upper stages and satellite. Flight successful. - . Nation: Europe. Agency: ELDO. Apogee: 120 km (70 mi).

1967 November 14 - . LV Family: N1. Launch Vehicle: N1.
  • N1-L3 moon landing schedule revised. - . Nation: USSR. Spacecraft: Soyuz 7K-LOK; LK. Summary: Decree 'On revision of the timetable for the N1-L3' was issued..

1967 November 14 - . 05:27 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 7C. LV Configuration: Skylark-7C SL423.
  • B field / Ultraviolet Abs Ionosphere mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 178 km (110 mi).

1967 November 14 - . 10:05 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.229UG.
  • Ultraviolet stellar spectra Ultraviolet astronomy mission - . Nation: USA. Agency: NASA; NRL. Apogee: 172 km (106 mi).

1967 November 14 - . 14:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF07. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 1215.
  • FOT GB51 Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 November 14 - . 15:22 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF09. Launch Pad: LF09?. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 1028.
  • FOT GB52 Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1968 November 14 - .
  • Zond 6 passes behind moon. - . Nation: USSR. Related Persons: Mishin; Leonov; Sevastyanov. Program: Lunar L1. Flight: Soyuz 7K-L1 mission 1. Spacecraft: Soyuz 7K-L1. The L1 went behind the moon at 05:49:37, and emerges at 06:21:11. At the time of the next orientation session it is 390,000 km from the earth and moving at 0.6 km/s. All orientations have been made on Sirius so far. Two more are needed: one for the midcourse correction, and then the second for the guided re-entry. The 100K sensor has proven itself despite Kamanin's doubts. Mishin's grumbly voice was grating on everyone, and finally he was put to bed. Kamanin despairs that the Soviet space program is dependent on this poorly organised, capricious, shortsighted man. Discussions are held with Moscow. If Apollo 8 succeeds, the next L1 test in January and the manned flight in April are probably not worth the risk. Some of the scientists want to discuss the inclusion of new medical experiments on pending manned spaceflights, but Kamanin is opposed to it. He does not want anything interfering with the primary mission. What to name the manned L1 spacecraft is discussed. Leonov wants to call it Rodina, Sevastyanov Ural, and Kamanin - 'Academician Korolev'.

1968 November 14 - . Launch Site: Green River. Launch Complex: Green River Pad 1. LV Family: Athena RTV. Launch Vehicle: Athena RTV. LV Configuration: Athena V120B.
  • USAF V120B re-entry vehicle test flight - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1969 November 14 - . 16:22 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Saturn V. Launch Vehicle: Saturn V. LV Configuration: Saturn V SA-507.
  • Apollo 12 - . Call Sign: Yankee Clipper. Crew: Bean; Conrad; Gordon. Backup Crew: Irwin; Scott; Worden. Payload: Apollo CSM 108 / Apollo LM 6 / ALSEP / S-IVB-507. Mass: 28,790 kg (63,470 lb). Nation: USA. Related Persons: Bean; Conrad; Gordon; Irwin; Scott; Worden. Agency: NASA Houston. Program: Apollo. Class: Moon. Type: Manned lunar spacecraft. Flight: Apollo 12. Spacecraft: Apollo CSM. Duration: 10.19 days. Decay Date: 1969-11-24 . USAF Sat Cat: 4225 . COSPAR: 1969-099A. Apogee: 186 km (115 mi). Perigee: 181 km (112 mi). Inclination: 32.5000 deg. Period: 88.19 min. 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.

  • Apollo 12 LM - . Call Sign: Intrepid. Payload: Apollo LM 6. Mass: 15,223 kg (33,560 lb). Nation: USA. Agency: NASA Houston. Program: Apollo. Class: Moon. Type: Manned lunar spacecraft. Flight: Apollo 12. Spacecraft: Apollo LM. Duration: 10.19 days. Decay Date: 1969-11-24 . USAF Sat Cat: 4225 . COSPAR: 1969-099x. Apogee: 186 km (115 mi). Perigee: 181 km (112 mi). Inclination: 32.5000 deg. Period: 88.19 min.

1970 November 14 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • OLD FOX 03M demonstration and shakedown operations launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1971 November 14 - .
  • Mariner 9, Mars Orbit Insertion - . Nation: USA. Spacecraft: Mariner 8-9.

1972 November 14 - . 18:48 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.02GS.
  • Solar mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1973 November 14 - . 20:40 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Molniya 1-25 - . Payload: Molniya-1. Mass: 1,600 kg (3,500 lb). Nation: USSR. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-1. Decay Date: 1979-05-26 . USAF Sat Cat: 6932 . COSPAR: 1973-089A. Apogee: 39,607 km (24,610 mi). Perigee: 461 km (286 mi). Inclination: 64.0000 deg. Period: 712.00 min. Summary: Operation of a system of long range telephone-telegraph radiocommunication, and transmission of USSR Central Television programmes to the stations of the Orbita network. .

1974 November 14 - . 09:46 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy/Ionosphere/Chemical release/Plasma mission - . Nation: USSR. Apogee: 150 km (90 mi).

1975 November 14 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT50GM Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1975 November 14 - . 19:14 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Molniya 3-03 - . Payload: Molniya-3 s/n 13. Mass: 1,600 kg (3,500 lb). Nation: USSR. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-3. USAF Sat Cat: 8425 . COSPAR: 1975-105A. Apogee: 38,527 km (23,939 mi). Perigee: 1,823 km (1,132 mi). Inclination: 63.9000 deg. Period: 717.70 min. Continued operation of the long-range telephone and telegraph radio-communication system within the Soviet Union and transmission of USSR central television programmes to stations in the Orbita and participating international networks (international cooperation scheme).

1976 November 14 - . 10:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: PRILIV. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 60 km (37 mi).

1977 November 14 - .
  • Kamanin still keeping his diary. - . Nation: USSR. Summary: Kamanin looks back at celebrations for the 60th Anniversary of the October Revolution. He notes that Soyuz 25 failed to dock..

1978 November 14 - . 14:00 GMT - . Launch Site: Fort Sherman. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 63 km (39 mi).

1979 November 14 - . Launch Site: Kourou. Launch Complex: Kourou ALFS. LV Family: Stromboli. Launch Vehicle: Eridan. LV Configuration: Eridan E016.
  • Ariane range test - . Nation: France. Agency: CNES. Apogee: 350 km (210 mi).

1980 November 14 - . 20:00 GMT - . Launch Site: ETR Launch Area. Launch Platform: UK S26. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3TK.
  • Chevaline warhead test launch - . Nation: UK. Agency: RN. Apogee: 1,000 km (600 mi).

1981 November 14 - . 20:20 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 90 km (55 mi).

1981 November 14 - .
  • Landing of STS-2 - . Return Crew: Engle; Truly. Nation: USA. Related Persons: Engle; Truly. Program: STS. Flight: STS-2. Summary: STS-2 landed at 21:23 GMT. .

1982 November 14 - . 07:55 GMT - . Launch Site: Poker Flat. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.01UE.
  • ARCS 2 Plasma mission - . Nation: USA. Agency: NASA. Apogee: 473 km (293 mi).

1982 November 14 - . 17:00 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 632. LV Family: Trident. Launch Vehicle: Trident C-4.
  • Demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1983 November 14 - . 12:45 GMT - . Launch Site: Wallops Island. LV Family: Loki. Launch Vehicle: Loki Dart. LV Configuration: Loki Dart T 1-0781.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 61 km (37 mi).

1984 November 14 - .
  • EVA STS-51-A-2 - . Crew: Allen; Gardner. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.25 days. Nation: USA. Related Persons: Allen; Gardner. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-51-A. Spacecraft: Discovery. Summary: Retrieved Westar satellite..

1984 November 14 - . 00:34 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 3914. LV Configuration: Delta 3914 D177.
  • NATO 3D - . Mass: 320 kg (700 lb). Nation: NATO. Agency: NATO. Program: NATO. Class: Communications. Type: Military communications satellite. Spacecraft: NATO 3. USAF Sat Cat: 15391 . COSPAR: 1984-115A. Apogee: 35,796 km (22,242 mi). Perigee: 35,779 km (22,231 mi). Inclination: 2.2000 deg. Period: 1,436.20 min. Stationed at 138 deg W. Positioned in geosynchronous orbit at 30 deg W in 1985; 50 deg W in 1985-1986; 21 deg W in 1986-1991; 30 deg W in 1991-1993; 21 deg W in1993-1997; 18 deg W in 1997-1999 As of 31 August 2001 located at 19.33 deg W drifting at 0.021 deg W per day. As of 2007 Mar 10 located at 120.20W drifting at 19.149W degrees per day.

1984 November 14 - . 07:40 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1608 - . Payload: Yantar-1KFT no. 4. Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Cartographic satellite. Spacecraft: Yantar-1KFT. Duration: 33.00 days. Decay Date: 1984-12-17 . USAF Sat Cat: 15393 . COSPAR: 1984-116A. Apogee: 248 km (154 mi). Perigee: 195 km (121 mi). Inclination: 70.0000 deg. Period: 88.90 min. Summary: Military topographic / cartographic satellite..

1984 November 14 - . 12:20 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1609 - . 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: 1984-11-28 . USAF Sat Cat: 15395 . COSPAR: 1984-117A. Apogee: 354 km (219 mi). Perigee: 195 km (121 mi). Inclination: 72.9000 deg. Period: 90.00 min. Summary: Military cartographic satellite; returned film capsule..

1986 November 14 - . 00:23 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout G. LV Configuration: Scout G-1 S199C.
  • Polar Bear - . Payload: Transit O-16 / P 87-1. Mass: 125 kg (275 lb). Nation: USA. Agency: USAF STP. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Transit. USAF Sat Cat: 17070 . COSPAR: 1986-088A. Apogee: 1,013 km (629 mi). Perigee: 955 km (593 mi). Inclination: 89.6000 deg. Period: 104.80 min. Tranist O-17 had been turned over to the National Air and Space Museum in 1976 and was displayed to the public for more than 8 years. In 1984, it was refurbished at APL and launched as the Polar Beacon Experiment and Auroral Research satellite to collect data for studying communications over the Earth’s polar regions.

1987 November 14 - . 09:29 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1896 - . Payload: Yantar-1KFT no. 8. Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Cartographic satellite. Spacecraft: Yantar-1KFT. Duration: 41.00 days. Decay Date: 1987-12-25 . USAF Sat Cat: 18535 . COSPAR: 1987-093A. Apogee: 263 km (163 mi). Perigee: 206 km (128 mi). Inclination: 64.8000 deg. Period: 89.20 min. Summary: Military topographic / cartographic satellite..

1987 November 14 - . 14:10 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 N. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.030UH.
  • X-ray astronomy mission - . Nation: USA. Agency: NASA. Apogee: 300 km (180 mi).

1988 November 14 - . 07:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: PASSAT. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 62 km (38 mi).

1990 November 14 - . 06:33 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 2103 - . 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: 1991-04-03 . USAF Sat Cat: 20933 . COSPAR: 1990-096A. Apogee: 415 km (257 mi). Perigee: 402 km (249 mi). Inclination: 65.0000 deg. Period: 92.70 min. Summary: Ocean surveillance..

1994 November 14 - .
1995 November 14 - . 17:04 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 N. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.127UG.
1997 November 14 - . 05:00 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.080UG.
  • SCARI 1 Ultraviolet astronomy mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

2000 November 14 - .
  • ISS Status Report: ISS 00-56 - . Nation: USA. Related Persons: Gidzenko; Shepherd. Program: ISS. Flight: ISS EO-1. Summary: The Expedition One crew continued work today to make the International Space Station a home, and to prepare for the arrival of a Russian cargo ship later this week.. Additional Details: ISS Status Report: ISS 00-56.

2002 November 14 - . 19:25 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF7632. LV Family: R-17. Launch Vehicle: R-17. LV Configuration: Scud FMA.
  • GMDS - . Nation: USA. Agency: MDA. Apogee: 46 km (28 mi).

2003 November 14 - . Launch Site: Mojave. Launch Complex: Mojave RW12/30. Launch Platform: W-Knight. Launch Vehicle: Tier One.
  • White Knight/SpaceShipOne Flight 40L/08G - . Crew: Siebold. Nation: USA. Related Persons: Melvill; Binnie; Siebold. Agency: Scaled. Program: X-Prize. Spacecraft: SpaceShipOne. Objectives: The fifth glide flight of SpaceShipOne. New pilot checkout flight. Stability and control testing with the new extended horizontal tails. Tests included stall performance at aft limit CG and evaluation of the increased pitch and roll control authority. Other objectives included additional testing of the motor controller (MCS) and handling qualities in feathered flight. Results: Launch conditions were 47,300 feet and 115 knots. Satisfactory stability and control at aft limit CG. A notable improvement in control power, particularly in roll. Handling qualities into and out of feather remained excellent with good nose pointing ability. Adjusted landing pattern altitudes resulted in a touchdown at the targeted runway aim-point.

    Flight Time: 1.4 hours / 19 mins 55 secs White Knight Pilot: Binnie White Knight Copilot: Stinemetze White Knight Flt Engineer: SpaceShipOne Pilot: Siebold High Chase-Starship Pilot: Karkow Low Chase-Duchess Pilot: Melvill/ Coleman


2003 November 14 - . 16:01 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-8 (74).
  • Zhongxing 20 - . Payload: Feng Huo 2. Mass: 2,300 kg (5,000 lb). Nation: China. Agency: SISE. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: DFH-3. USAF Sat Cat: 28082 . COSPAR: 2003-052A. Apogee: 35,811 km (22,251 mi). Perigee: 35,762 km (22,221 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Military communications satellite. As of 2007 Mar 11 located at 103.00E drifting at 0.010W degrees per day..

2005 November 14 - . 20:30 GMT - . Launch Site: White Sands. LV Family: Terrier. Launch Vehicle: Terrier Orion Improved. LV Configuration: Terrier Improved Orion NASA 41.66DR.
  • Target - . Nation: USA. Agency: NASA; NAWC. Apogee: 130 km (80 mi).

2007 November 14 - . 22:06 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA V179 (538).
  • Skynet 5B - . Mass: 4,635 kg (10,218 lb). Nation: UK. Agency: Paradigm. Program: Skynet. Class: Communications. Type: Military communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 32294 . COSPAR: 2007-056B. Apogee: 35,789 km (22,238 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Skynet 5B was designed to provide communications services in the SHF and UHF bands to the UK Ministry of Defence..
  • Star One C1 - . Nation: Brazil. Agency: Embratel. Program: Brasilsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 32293 . COSPAR: 2007-056A. Apogee: 35,780 km (22,230 mi). Perigee: 35,794 km (22,241 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Formerly named Brasilsat C1, the satellite was launched as part of a joint venture between several South American countries with Brazil's Embratel taking a lead role..

2008 November 14 - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 9.
  • NASA 36.221DS - . Nation: USA. Summary: Solar astronomy payload..

2008 November 14 - . 15:50 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2445 - . Nation: Russia. Agency: KVR. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Decay Date: 2009-02-23 . USAF Sat Cat: 33439 . COSPAR: 2008-058A. Apogee: 327 km (203 mi). Perigee: 181 km (112 mi). Inclination: 67.2000 deg. Period: 89.60 min. Summary: Recoverable reconnaisance satellite. Launched annually since 2005 with a typical 75 to 100 day mission, with recovery on an interim basis of two film capsules and final deorbiting of the camera and main film magazine..

2009 November 14 - . 02:30 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 9.
  • NASA 36.252UH - . Nation: USA. Agency: NASA Greenbelt. Summary: X-ray astronomy payload. X-ray spectroscopy instrument scanned the Cygnus Loop region..

2010 November 14 - . 17:29 GMT - . Launch Site: Baikonur. LV Family: Proton. Launch Vehicle: Proton/Briz M.
  • Skyterra 1 - . Mass: 5,400 kg (11,900 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: HS 702. USAF Sat Cat: 37218 . COSPAR: 2010-061A. Apogee: 35,802 km (22,246 mi). Perigee: 35,772 km (22,227 mi). Inclination: 6.0000 deg. Period: 1,436.10 min. Summary: GeoMobile class satellite with a 22-meter L-band reflector..

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