Encyclopedia Astronautica
November 13


November 13 Chronology


1907 November 13 - .
  • Birth of Kenneth D Nichols - . Nation: USA. Summary: American manager, involved in directing the guided missile research and development effort for the Secretary of Defense in the early 1950's..

1931 November 13 - .
  • Birth of John A Manke - . Nation: USA. Summary: American NASA test pilot 1962-1981. Flew record 42 lifting body rocketplane missions..

1944 November 13 - . Launch Site: V-2 Battery SS Abt 500. LV Family: V-2. Launch Vehicle: V-2.
  • SS V-2 Battery 500 begins transfer from Burgsteinfurt to Hellendoorn, Archem, Holland. - . Nation: Germany. Agency: Wehrmacht.

1947 November 13 - . 08:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: V-2. Launch Vehicle: A-4. LV Configuration: A-4 22N.
  • Soviet V-2 launch - . Nation: USSR. Agency: Korolev. Apogee: 89 km (55 mi).

1947 November 13 - . 14:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: V-2. Launch Vehicle: A-4. LV Configuration: A-4 19N.
  • Soviet V-2 launch - . Nation: USSR. Agency: Korolev. Apogee: 89 km (55 mi). Summary: Range achieved 270 km. Broke up on re-entry..

1948 November 13 - .
  • British Interplanetary Society's H. E. Ross described a manned satellite station. - . Nation: UK. Spacecraft: BIS Station. In a paper presented to the British Interplanetary Society, H. E. Ross described a manned satellite station in Earth orbit that would serve as an astronomical and zero-gravity and vacuum research laboratory. (Ross' bold suggestions also included schemes for a manned landing on the Moon and return to Earth through use of the rendezvous technique in Earth orbit and about the Moon.) Ross' suggested design comprised a circular structure that housed the crew of the space laboratory (numbering 24 specialists and support personnel) as well as telescopes and research equipment. The station, he suggested, could be resupplied with oxygen and other life-support essentials by supply ships launched every three months.

1948 November 13 - .
  • British Interplanetary Society manned lunar landing mission - . Nation: UK. Spacecraft: BIS Lunar Lander. A paper read to the British Interplanetary Society by H. E. Ross described a manned lunar landing mission which would require a combination of the earth orbit and lunar orbit rendezvous techniques. Three spacecraft would be launched simultaneously into earth orbit, each carrying a pilot. After rendezvous, the crew would transfer to ship A, which would refuel from ships B and C. Ship C would be discarded completely, but ship B would be fueled with the surplus not needed by A. The spacecraft would then be fired into a translunar trajectory. Upon reaching the vicinity of the moon, the spacecraft would go into lunar orbit, detach fuel tanks, and descend to the lunar surface. To return to earth, the spacecraft would rendezvous with the fuel tanks, refuel, and fire into a transearth trajectory. On approaching the earth, the spacecraft would rendezvous with ship B, the crew would transfer to ship B, and descend to earth. The ability to rendezvous in space was seen to be the essential element of such a project. The total payload weight at launch would be 1,326 tons equally divided among the three ships as compared to 2.6 times this weight required for a direct ascent and return from the moon.

1951 November 13 - . Launch Site: White Sands. LV Family: Honest John. Launch Vehicle: Honest John. LV Configuration: Honest John 13.
  • Test mission - . Nation: USA. Apogee: 10 km (6 mi).

1952 November 13 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bechar. LV Family: Veronique. Launch Vehicle: Veronique. LV Configuration: Veronique N7. FAILURE: Failure.
  • Test mission - . Nation: France. Agency: LRBA. Apogee: 4.00 km (2.40 mi).

1953 November 13 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1225A.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1957 November 13 - . 11:52 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 1. LV Configuration: Skylark-1 SL04.
  • Grenade / Chaff / Sodium release Test / aeronomy mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 127 km (78 mi).

1957 November 13 - . 17:28 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC9. LV Family: Navaho. Launch Vehicle: Navaho G-26. LV Configuration: Navaho II SM-64 11. FAILURE: Destroyed by range safety after telemetry dropped out at T+75 seconds.
  • Navaho G-26 Flight 7 - . Nation: USA. Agency: USAF. Apogee: 20 km (12 mi). The booster functioned well, and the cruise stage separated at 20.4 km altitude and Mach 3.24. The ramjets ignited, but before the ground knew that, the telemetry dropped out completely due to a faulty voltage regulator on the missile. Range safety ordered the missile's self destruction at T+75 seconds.

1958 November 13 - . 08:59 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun CC6.02.
  • Infrared airglow Aeronomy mission - . Nation: Canada. Agency: CARDE. Apogee: 142 km (88 mi).

1958 November 13 - . 17:34 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun OB6.13.
  • Arctic cloud cover Meteorological / imaging mission - . Nation: USA. Agency: USAF. Apogee: 119 km (73 mi).

1960 November 13 - . 16:03 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.16GE.
  • SBE 10 (LE SCR) Magnetosphere mission - . Nation: USA. Agency: NASA. Apogee: 129 km (80 mi).

1961 November 13 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bacchus. LV Family: VE. Launch Vehicle: Agate.
  • Test mission - . Nation: France. Agency: ONERA. Apogee: 20 km (12 mi).

1962 November 13 - . LV Family: Atlas. Launch Vehicle: Atlas D.
  • Cooper named for Mercury MA-9 1-day orbital mission - . Nation: USA. Related Persons: Cooper; Shepard. Program: Mercury. Flight: Mercury MA-9. Summary: Gordon Cooper was named as the pilot for Mercury-Atlas 9 (MA-9) 1-day orbital mission slated for April 1963. Alan Shepard, pilot of Mercury-Redstone 3 (MR-3) was designated as backup pilot..

1962 November 13 - . 10:10 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 7C. LV Configuration: Skylark-7C SL114.
  • Solar X-rays / Meteors / O3 Solar / aeronomy / chemica mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 206 km (128 mi).

1962 November 13 - . 22:30 GMT - . Launch Site: Eglin. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 AC3.453.
  • Firefly III GILDA Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 253 km (157 mi).

1963 November 13 - . LV Family: N1. Launch Vehicle: N1.
  • N1 launch site facility construction approved. - . Nation: USSR. Summary: Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On approval of the schedule of work for the N1 launch complexes' was issued..

1963 November 13 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 446.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 November 13 - . 22:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 158D. FAILURE: Failure. Failed Stage: 1.
  • ST COOL WATER VI test - . Nation: USA. Agency: USAF SAC. Apogee: 100 km (60 mi).

1963 November 13 - . 23:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 AD3.324.
  • Dayglow Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 262 km (162 mi).

1964 November 13 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 633. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-87.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1964 November 13 - . Launch Site: Barking Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-65.
  • Ballistic Aeronomy mission - . Nation: USA. Agency: Sandia. Apogee: 308 km (191 mi).

1965 November 13 - . LV Family: Proton. Launch Vehicle: Proton.
  • Industrial orders to cancel LK-1 spacecraft and implement L1. - . Nation: USSR. Spacecraft: Soyuz 7K-L1; LK-1. Summary: Ministry of General Machine Building (MOM) Decree 'On work on the UR-500K-L1 program' was issued..

1966 November 13 - . 15:34 GMT - .
  • EVA Gemini 12-2 - . Crew: Aldrin. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.0896 days. Nation: USA. Related Persons: Aldrin. Program: Gemini. Class: Manned. Type: Manned spacecraft. Flight: Gemini 12. Spacecraft: Gemini. Summary: Tested tools and techniques for extravehicular activity..

1967 November 13 - . LV Family: N1; Saturn V.
  • Kamanin's thoughts on first Saturn V launch. - . Nation: USSR. Related Persons: Mishin; Ustinov; Smirnov; Pashkov; Malinovskiy; Grechko, Andrei. Program: Lunar L3; Apollo. The first Saturn V and Surveyor 6 have been launched by the Americans. Kamanin catalogues why the Americans are beating them: bad organisation, on the parts of Ustinov, Smirnov, Pashkov, Malinovskiy, and Grechko; technical errors and an undisciplined approach to the fulfilment of government decrees concerning the Soyuz and N1 on the parts of Chief Designers Korolev and Mishin; lack of coordination between the institutes and design bureaux compared to the United States; and finally, the Americans are spending several times more money than has been dedicated to the Soviet space program.

1968 November 13 - .
  • HL-10 Flight 13 - . Crew: Manke. Payload: HL-10 flight 13. Nation: USA. Related Persons: Manke. Program: NASA Lifting Body. Class: Manned. Type: Manned spaceplane. Spacecraft: HL-10. Summary: 2 chambers, 186-sec powered flight. Maximum Speed - 843 kph. Maximum Altitude - 13000 m. Flight Time - 385 sec..

1968 November 13 - .
  • Zond 6 midcourse correction. - . Nation: USSR. Related Persons: Ustinov; Mishin; Tyulin; Korolev. Program: Lunar L1. Flight: Soyuz 7K-L1 mission 1. Spacecraft: Soyuz 7K-L1. Tracking of the L1 shows it will hit the earth on return, but without a further midcourse correction the perigee will be 200 km instead of the 45 km required. Therefore another correction will be needed on the way back from the moon. Ustinov calls a meeting and asks 'How do we answer Apollo 8?'. The reply of Mishin and Tyulin is that 'we are not ready to answer Apollo 8. Apollo 8 is a high-risk adventure. The Americans have not accomplished any unmanned lunar flybys to demonstrate that their systems will function correctly; and of only two Saturn V flight tests to date, the second was a failure. We need to make the L1 program public to show the seriousness and completeness of Soviet readiness'. Ustinov orders the following plan be carried out in the next two months: in December, one unmanned L1 flight, and the first launch of the N1 with an L3 mock-up. In January 1969, a lunar flyby with two cosmonauts; a Lunokhod robot rover will be placed on the lunar surface; and a dual Soyuz manned flight with 1+3 crewmembers. Kamanin notes that the problem with the technical approach of Korolev and Mishin is that cosmonauts are seen only as observers and back-ups to automated systems. Therefore the whole manned space program is based on a false assumption. Because of this the Soviets have lost 2-3 years in the space race, which would have been saved if they had followed the Gemini/Apollo 'pilot in the loop' approach. Afterwards Mishin meets with the L1 cosmonaut group. He wants to get rid of the on-board flight plan and reduce the manual for operation of the spacecraft to one page. 'Don't want to bring bureaucracy aboard the spacecraft' he says. This completely absurd idea again demonstrates his belief in total reliance on automated systems.

1968 November 13 - . 12:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 253 - . Payload: Zenit-2 11F61 s/n 67. Mass: 4,720 kg (10,400 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2. Duration: 5.00 days. Decay Date: 1968-11-18 . USAF Sat Cat: 3542 . COSPAR: 1968-102A. Apogee: 337 km (209 mi). Perigee: 216 km (134 mi). Inclination: 65.4000 deg. Period: 90.00 min. Summary: Area survey photo reconnaissance satellite. Unsuccessful mission. On 13th orbit the SA-20-1 camera's shutter responded to an uncommanded order to open. Radiation levels inside reached 3 times normal levels. 53% of the data was lost..

1968 November 13 - . 12:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2537.
  • Giant Fist 5 demonstration and shakedown operations launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1969 November 13 - .
1969 November 13 - .
  • X-24 Flight 7 - . Crew: Gentry. Payload: X-24A flight 7. Nation: USA. Related Persons: Gentry. Class: Manned. Type: Manned spaceplane. Spacecraft: X-24A. Summary: Glide. Maximum Speed - 687 kph. Maximum Altitude - 13720 m. Flight Time - 270 sec..

1970 November 13 - . LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Shuttle specifications revised - . Nation: USA. Summary: Further minor changes were made as a result of the NASA 90-day review in October..

1970 November 13 - . 22:19 GMT - . Launch Site: Andoya. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.115IE.
  • Ferdinand 23 Auroral mission - . Nation: USA. Agency: NASA. Apogee: 214 km (132 mi).

1972 November 13 - . 14:04 GMT - . Launch Site: Antigua. Launch Vehicle: Rocketsonde.
  • Met Para, Arcasonde - . Nation: USA. Agency: MRN. Apogee: 61 km (37 mi).

1973 November 13 - . 09:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKMR. Launch Platform: NOKV. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 88 km (54 mi).

1974 November 13 - .
  • Birth of Sergei Nikolayevich Ryazansky - . Nation: Russia. Summary: Russian physician cosmonaut, 2003-on. Worked at IMBP, in the post of senior scientific researcher at the "Sensomotornoy, Fiziology i Profilaktiky" department. Cosmonaut training 16 June 2003 - 27 June 2005..

1974 November 13 - . 14:00 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 95 km (59 mi).

1975 November 13 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 642. Launch Vehicle: Poseidon.
  • FOT-16? Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1975 November 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SFT-16 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1976 November 13 - . 10:31 GMT - . Launch Site: Poker Flat. LV Family: Honest John. Launch Vehicle: HJ Nike Hydac. LV Configuration: HJ Nike Hydac ARPA WS614.51-3.
  • WIDEBAND Ionosphere mission - . Nation: USA. Agency: DARPA. Apogee: 500 km (310 mi).

1977 November 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES TDV-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1977 November 13 - . 08:55 GMT - . Launch Site: Poker Flat. LV Family: Sergeant. Launch Vehicle: Sounding Rocket. LV Configuration: Sergeant DNA IC730.09-1.
  • FWIF I Aeronomy / aurora / solar mission - . Nation: USA. Agency: DNA. Apogee: 141 km (87 mi).

1978 November 13 - . 05:24 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas Centaur SLV-3D. LV Configuration: SLV-3D Centaur AC-52 / Centaur D-1AR 5032.
  • HEAO 2 - . Payload: HEAO B. Mass: 3,150 kg (6,940 lb). Nation: USA. Agency: NASA Huntsville. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: HEAO. Decay Date: 1982-03-25 . USAF Sat Cat: 11101 . COSPAR: 1978-103A. Apogee: 548 km (340 mi). Perigee: 526 km (326 mi). Inclination: 23.5000 deg. Period: 95.40 min. Summary: High Energy Astronomy Observatory. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C)..

1978 November 13 - . 12:44 GMT - . Launch Site: Poker Flat. LV Family: Sergeant. Launch Vehicle: Sounding Rocket. LV Configuration: Sergeant DNA IC830.09-1A.
  • FWIF II Auroral Infrared mission - . Nation: USA. Agency: DNA. Apogee: 141 km (87 mi).

1979 November 13 - . 04:45 GMT - . Launch Site: Poker Flat. LV Family: Strypi. Launch Vehicle: Strypi. LV Configuration: Strypi NASA 12.37UE.
  • ECHO V Auroral mission - . Nation: USA. Agency: NASA. Apogee: 215 km (133 mi).

1980 November 13 - . 20:37 GMT - . Launch Site: Point Mugu. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 90 km (55 mi).

1981 November 13 - . 09:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1319 - . 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: 1981-11-27 . USAF Sat Cat: 12954 . COSPAR: 1981-112A. Apogee: 374 km (232 mi). Perigee: 204 km (126 mi). Inclination: 70.4000 deg. Period: 90.30 min. Summary: Photo surveillance; returned film capsule..

1982 November 13 - . 12:45 GMT - . Launch Site: Point Mugu. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 89 km (55 mi).

1984 November 13 - . Launch Site: Western Test Range DZ. Launch Pad: 35.0 N x 120.0 W. Launch Platform: F-15. Launch Vehicle: ASAT.
  • ASAT Test - . Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). Summary: Failed test; minitaure homing vehicle was to home on a selected star..

1984 November 13 - . Launch Site: Baikonur. LV Family: R-36M. Launch Vehicle: R-36M.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1984 November 13 - . Launch Site: Baikonur. LV Family: MR-UR-100. Launch Vehicle: Perimetr 15A11.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1985 November 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-10.
  • 4 RVs Test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1985 November 13 - . 12:25 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1702 - . 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: 1985-11-27 . USAF Sat Cat: 16247 . COSPAR: 1985-106A. Apogee: 370 km (220 mi). Perigee: 192 km (119 mi). Inclination: 72.9000 deg. Period: 90.10 min. Summary: Military cartographic satellite; returned film capsule..

1986 November 13 - . 06:10 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53748-414.
  • Cosmos 1791 - . Payload: Tsikada. Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Tsikada. USAF Sat Cat: 17066 . COSPAR: 1986-086A. Apogee: 1,010 km (620 mi). Perigee: 951 km (590 mi). Inclination: 83.0000 deg. Period: 104.70 min. Summary: Replaced Cosmos 1553. Civilian navigation satellite. Positioned in plane 11 of constellation..

1986 November 13 - . 10:59 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1792 - . Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 53.00 days. Decay Date: 1987-01-05 . USAF Sat Cat: 17068 . COSPAR: 1986-087A. Apogee: 309 km (192 mi). Perigee: 184 km (114 mi). Inclination: 64.9000 deg. Period: 89.40 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..

1987 November 13 - . 12:58 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHIR. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 81 km (50 mi).

1989 November 13 - . 14:07 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 83 km (51 mi).

1990 November 13 - . 00:37 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. LV Family: Titan. Launch Vehicle: Titan 402A/IUS. LV Configuration: Titan 402A/IUS K-6 (45D-2).
  • USA 65 - . Payload: DSP-1 Block 14 F15. Mass: 2,360 kg (5,200 lb). Nation: USA. Agency: USAF. Class: Military. Type: Early warning satellite. Spacecraft: DSP. Completed Operations Date: 2006-01-01 . USAF Sat Cat: 20929 . COSPAR: 1990-095A. Apogee: 35,699 km (22,182 mi). Perigee: 35,614 km (22,129 mi). Inclination: 3.1000 deg. Period: 1,421.80 min. Summary: DSP-1 Block 14 ballistic missile launch detection satellite. Positioned in geosynchronous orbit at 105 deg E in 1991; 70 deg E in 1991-1992; 5 deg E in 1992-1993; 35 deg W in 1993; 38 deg W in 1999-2004. Believed to have been taken out of service in 2006..

1991 November 13 - . 15:21 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 73 km (45 mi).

1994 November 13 - .
  • Mir News 239: Progress-M25 docked at Mir-space station. - . Nation: Russia. Program: Mir. Flight: Mir EO-17; Mir LD-4. The freighter P-M25 docked at Mir's aft (Kvant-1) docking port on 13.11.94 at 0904 UTC (during orb. 49926). The approach and docking took place in the automatic mode by the system Kurs. On board Soyuz-TM20 Viktorenko was standby with the system TORU, but manual interference was not necessary. The operation could be monitored via Altair between 0822 and 0904 UTC. During the next pass (orb. 49927, 1027 UTC) the gentlemen on board left the honour to give the first post-docking report to Yelena Kondakova. Enthusiastically she reported the airseal, the opening of the hatch, the fact that Progress-M25 was clean and that they enjoyed the nice smell of apples and lemons. Polyakov said that the Progress-M25 was an ideal freighter.

    Progress-M25 delivered to the Mir-station new supplies of water, fuel, food, spare parts for repair (among which parts for the furnace to be used for the conclusion of the Euromir94 materials processing experiments) and post. Progress-M25 has not been equipped by a VBK (Ballistic Return Capsule).

    Jubilees: In the early morning of 18.11.94 Mir -that is to say the first part, the base block, launched on 19.02.1986- will make her 50000th orbit around the Earth. From that early beginning I tried to monitor as much as possible all passes within range. If I was a robot and had been able to monitor all passes this number would be 12500. But not being a robot I needed holidays etc. Nevertheless at a rough estimation I must have been monitoring Mir's radio traffic during 10000 passes. Homage to my poor ear-drums!

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


1994 November 13 - .
  • Death of Richard V Rhode - . Nation: USA. Related Persons: Rhode. Summary: American engineer, at NASA 1925-1967, involved with air and launch vehicle research and advanced design criteria..

1996 November 13 - . 18:30 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 36.142GS.
  • SERTS-96 (07) Solar extreme ultraviolet mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

1996 November 13 - . 22:40 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L-3 V92.
  • Arabsat 2B - . Nation: Arab States. Agency: Arabsat. Manufacturer: Cannes. Program: Arabsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 24652 . COSPAR: 1996-063A. Apogee: 35,788 km (22,237 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Geostationary at 21.9E. Positioned in geosynchronous orbit at 30 deg E in 1997-1999 As of 4 September 2001 located at 30.46 deg E drifting at 0.009 deg E per day. As of 2007 Mar 10 located at 30.52E drifting at 0.005E degrees per day..
  • Measat 2 - . Nation: Malaysia. Agency: Binarian. Program: Measat. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 376. USAF Sat Cat: 24653 . COSPAR: 1996-063B. Apogee: 35,792 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Geostationary at 148.0E. Positioned in geosynchronous orbit at 148 deg E in 1996-1999 As of 5 September 2001 located at 148.00 deg E drifting at 0.011 deg W per day. As of 2007 Mar 9 located at 147.98E drifting at 0.007W degrees per day..

1999 November 13 - .
  • Test Pilot John Paul Stapp dies at age of 89 -- Natural causes. - . Nation: USA. Related Persons: Stapp. Summary: American USAF flight surgeon. In 1946-1958 pioneer research with rocket sleds and balloons; defined human tolerances for G-forces, altitude, and blast, essential data for design of aerospacecraft. Personally underwent the most grueling tests..

1999 November 13 - . 08:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-01.
  • PRP FTM-01 test - . Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi).

1999 November 13 - . 22:54 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP-3 V123.
  • GE 4 - . Nation: USA. Agency: GE Americom. Manufacturer: Lockheed. Program: Americom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 25954 . COSPAR: 1999-060A. Apogee: 35,793 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Provided C and Ku-band communications services for GE Americom, replacing Spacenet 4. Stationed at 101 deg W. Positioned in geosynchronous orbit at 74 deg W in 1999. As of 5 September 2001 located at 101.12 deg W drifting at 0.008 deg W per day. As of 2007 Mar 11 located at 101.02W drifting at 0.004W degrees per day.

2001 November 13 - . 21:41 GMT - .
  • EVA ISS EO-3-3 - . Crew: Culbertson; Dezhurov. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.22 days. Nation: USA. Related Persons: Culbertson; Dezhurov. Program: ISS. Class: Manned. Type: Manned spaceplane. Flight: ISS EO-3. Summary: The spacewalk was made from the Pirs module. The astronauts completed external connections for the module and finished setting up the Kurs rendezvous system. .

2006 November 13 - . Launch Site: Blue Origin. Launch Vehicle: New Shepard.
  • First test launch of New Shepard subscale prototype - . Nation: USA. Agency: Blue Origin. Class: Manned. Type: Manned rocketplane. Spacecraft: New Shepard. The test vehicle, dubbed Goddard, lifted off and landed vertically, and reached 90 m altitude. The launch, delayed twice for winds, came at the end of a three-day FAA-approved window. Video and pictures issued indicated that the test vehicle was a subscale (about 84%) version of the final manned vehicle; and that it used a hydrogen peroxide monopropellant rocket engines in place of the hydrogen peroxide/kerosene engines planned for the production vehicle.

2008 November 13 - .
  • Death of Gennadi Aleksandrovich Dolgopolov - . Nation: Russia. Related Persons: Dolgopolov. 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..

2008 November 13 - . 09:06 GMT - . Launch Site: Biscarosse. LV Family: MSBS. Launch Vehicle: MSBS M51.
Home - Browse - Contact
© / Conditions for Use