See also Born on this Day On this day in: 1930 - Launch Vehicle: Valier. -
Valier rocket car Nation: Germany. Valier has arranged for Dr Weyland to develop a new, powerful liquid rocket engine burning liquid oxygen and gasoline. The car made its first slow run this day, but combustion of the motor was poor and acceleration of the vehicle low.
1932 - Launch Vehicle: Goddard. Model: Goddard 4.
1948 - 19:54 GMT - Launch Site: White Sands. Launch Complex: LC33. Launch Pad: -. Launch Vehicle: V-2. LV Configuration: V-2 38. FAILURE: Failure.
1949 -
1958 - 13:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DM-18. LV Configuration: Thor DM-18 121. FAILURE: Failure. -
Research and development Series II test Nation: USA. Agency: USAF 6555 ATW. Apogee: 0 km ( mi).
1959 - Launch Site: Kapustin Yar. Launch Complex: VLAD. Launch Pad: -. Launch Vehicle: Burya. LV Configuration: Burya 2-05.
1960 - 14:15 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee Hi. LV Configuration: Aerobee Hi NN3.60. -
NN3.60 Pinhole camera Solar ultraviolet / solar extreme ultraviolet mission Nation: USA. Agency: NRL. Apogee: 222 km (137 mi).
1960 - 16:51 GMT - Launch Site: Rosamund Dry Lake DZ. Launch Complex: -. Launch Pad: 34.7 N x 118.1 W. Launch Vehicle: X-15. LV Configuration: X-15 1-5-10.
1961 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1E-20. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1961 - 09:36 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.05CA. -
Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 164 km (101 mi).
1961 - 18:37 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp ISRC-RS-02. -
Aeronomy mission Nation: Italy. Agency: ISRC. Apogee: 200 km (120 mi).
1962 - Launch Site: AMR DZ. Launch Complex: -. Launch Pad: 29.0 N x 79.0 W. Launch Vehicle: Skybolt. LV Configuration: Skybolt ALBM 20025. FAILURE: Failure. -
Test mission Nation: USA. Agency: USAF. Apogee: 10 km (6 mi).
1962 - 18:02 GMT - Launch Site: Mud Lake DZ. Launch Complex: -. Launch Pad: 37.9 N x 117.1 W. Launch Vehicle: X-15. LV Configuration: X-15 1-26-46.
1963 - -
Cosmonaut training for Vostok 5/6. Nation: USSR. Spacecraft: Vostok. Flight: Vostok 5, Vostok 6. It is clear that the female cosmonauts are trained and ready for an August flight, and the men (Bykovskiy, Volynov, Leonov, Khrunov) can complete training by that date. The male cosmonauts object to spending 7 to 8 days in a spacesuit in the ground spacecraft mock-up as required by the flight doctors. They don't want to spend more than 3 to 4 days.
1963 - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-21. FAILURE: Failure. -
Research and development test Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi). Mk 6 re-entry vehicle
1965 - 02:20 GMT - Launch Site: Baikonur. Launch Complex: LC130. Launch Pad: -. Launch Vehicle: UR-100. LV Configuration: UR-100 U106416-01. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1966 - 19:12 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3 Agena D. LV Configuration: SLV-3 Agena D 7117 / Agena D 7117.
1967 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -.
1967 - 06:14 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C87. -
ISRO 45.01 Ionosphere mission Nation: India. Agency: ISRO. Apogee: 128 km (79 mi).
1967 - 16:19 GMT - Launch Site: Kiruna. Launch Complex: C. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure 2B. LV Configuration: Centaure 2B CE-24/1. -
ESRO C24/1 test Nation: Europe. Agency: ESRO. Apogee: 123 km (76 mi).
1967 - 23:40 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk CRL AF08.650. -
Ba Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 260 km (160 mi).
1968 -
1969 - -
Military Soyuz meeting Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Kamanin meets with the General Staff, presents the results of the study he has commissioned on the military utility of manned spaceflight, and pleads for support for his proposal to procure ten Soyuz spacecraft.
1969 - 00:10 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Boosted Arcas 2. LV Configuration: Boosted Arcas 2 AMM-BA-1. -
O / OH profile Aeronomy mission Nation: Canada. Agency: Canada. Apogee: 104 km (64 mi).
1969 - 01:17 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Boosted Arcas 2. LV Configuration: Boosted Arcas 2 AMM-BA-2. -
O / OH profile Aeronomy mission Nation: Canada. Agency: Canada. Apogee: 103 km (64 mi).
1969 - 16:32 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Solar Extreme ultraviolet mission Nation: USSR. Agency: AN SSSR. Apogee: 174 km (108 mi).
1971 - 01:40 GMT - Launch Site: Baikonur. Launch Complex: LC81/24. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K. LV Configuration: Proton-K 254-01. -
Salyut 1 Nation: USSR. Program: Salyut. Payload: Zarya s/n 121. Mass: 18,500 kg (40,700 lb). Class: Manned. Type: Space station. Spacecraft: Salyut 1. Agency: MOM. Perigee: 180 km (110 mi). Apogee: 214 km (132 mi). Inclination: 51.40 deg. Period: 88.50 min. COSPAR: 1971-032A. USAF Sat Cat: 5160. Duration: 179.93 days. Decay Date: 1971-10-11. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. First manned space station. Salyut 1 included a number of military experiments, including the OD-4 optical visual ranger, the Orion ultraviolet instrument for characterising rocket plumes, and the highly classified Svinets radiometer. Primary objectives included photography of the earth, spectrographs of the earth's horizon, experiments with intense gamma rays, and studying manual methods for station orientation. At 05:20 the State Commission and their guests arrive at the Area 95 observation point to view the launch. The booster takes off on schedule at 06:40 in light rain and 60 km/hr wind. The tracking station reports good orbital insertion, separation from the third stage, and antennae and solar panel deployment. But the cover of the scientific equipment bay does not separate. This will mean that many experiments cannot be accomplished. It is decided to launch the crew to the station anyway, since the station is otherwise functioning normally. The cosmonauts go to the baths in the evening.
- Additional details.
1971 - 06:30 GMT - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena V127D. -
Re-entry Vehicle test Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).
1971 - 13:25 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.406IA. -
ISRO 10.41 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 198 km (123 mi).
1971 - 23:45 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3E-44. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1972 - 10:01 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Cockatoo. LV Configuration: Cockatoo 1027. -
Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi).
1972 - 21:43 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Delta. Model: Thorad SLV-2H Agena D. LV Configuration: Thorad SLV-2H Agena D 569 / Agena D 1661.
1973 - 08:59 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
1973 - 10:19 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/4. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
1974 - 04:30 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.520UI. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 199 km (123 mi).
1975 - 07:30 GMT - Launch Site: Kapustin Yar. Launch Complex: LC107/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53731-279.
1978 - 10:35 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 38.0 N x 75.0 W. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere mission Nation: USSR. Apogee: 161 km (100 mi).
1978 - 15:37 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 38.0 N x 75.0 W. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere mission Nation: USSR. Apogee: 170 km (100 mi).
1979 - Launch Site: Baikonur. Launch Complex: LC106. Launch Pad: -. Launch Vehicle: R-36M. -
DP Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1979 - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Malemute. LV Configuration: Malemute Sandia 497-009. -
Malemute II test Nation: USA. Agency: Sandia. Apogee: 165 km (102 mi).
1979 - Launch Site: Vandenberg. Launch Complex: LF21. Launch Pad: -. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-17. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).
1982 - 19:45 GMT - Launch Site: Baikonur. Launch Complex: LC200/40. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K. LV Configuration: Proton-K 306-02. -
Salyut 7 Nation: USSR. Program: Salyut 7. Payload: Zarya s/n 125-2. Mass: 18,900 kg (41,600 lb). Class: Manned. Type: Space station. Spacecraft: Salyut 7. Agency: MOM. Perigee: 279 km (173 mi). Apogee: 284 km (176 mi). Inclination: 51.60 deg. Period: 90.20 min. COSPAR: 1982-033A. USAF Sat Cat: 13138. Duration: 3,215.34 days. Decay Date: 1991-02-07. Second Soviet replenishable long-duration ‘civilian’ space station. Objectives: Continuation of scientific research on board manned space complexes in the interests of science and the Soviet national economy; testing of advanced systems and apparatus for orbital stations. Continuation of the scientific research in progress on board manned space complexes in the interests of science and the national economy; testing of advanced systems and apparatus for orbital stations. Although of the same design as Salyut 6, technical breakdowns throughout its life made Salyut 7 a much less productive station. Replaced finally by Mir. Two different TKS resupply craft, originally designed for the Almaz military station, docked with Salyut 7 to provide a larger complex. With the cancellation of Almaz, a large proportion of the experiments carried out on board had military objectives. As of January 1990 out of fuel, unable to manoeuvre, uncontrolled re-entry expected in three to four years. Re-entered in 1991 with 70 kg fuel remaining over Argentina. Controllers attempted to control impact point (set for Atlantic Ocean) by setting Salyut 7/Kosmos 1686 assembly into a tumble. This however failed and Salyut 7 re-entered February 7, 1991 04:00 GMT. Many fragments fell on the town of Capitan Bermudez, 25 km from Rosario and 400 km from Buenos Aires, Argentina. At 1 am local time the sky was lit up with hundreds of incandescent meteors travelling from Southwest to Northeast. At dawn the inhabitants discovered numerous metal fragments, which seemed to have fallen in distinct groups at various locations in the city. Luckily no one was hurt in the metallic shower.
- Additional details.
1983 - 12:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47119-520.
1983 - 20:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 GL A04.902. -
Ultraviolet Ionosphere / solar extreme ultraviolet mission Nation: USA. Agency: USAF. Apogee: 204 km (126 mi).
1984 - 11:40 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1985 - 14:00 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1985 -
1990 -
1992 - 21:29 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 R15000-059.
1993 - 05:50 GMT - Launch Site: Sriharikota. Launch Complex: -. Launch Pad: -. Launch Vehicle: RH. Model: RH-560. -
SPICE-3 Ionosphere mission Nation: India. Agency: ISRO. Apogee: 323 km (200 mi).
1993 - 17:15 GMT -
1995 - 21:50 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1998 - 13:51 GMT - Launch Site: Sriharikota. Launch Complex: -. Launch Pad: -. Launch Vehicle: RH. Model: RH-560/300 Mk II. -
DEOS F05 Ionosphere mission Nation: India. Agency: ISRO/DLR. Apogee: 433 km (269 mi).
2000 - 00:29 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 42L. LV Configuration: Ariane 42L-3 V129. -
Galaxy 4R Nation: USA. Program: Galaxy. Payload: Galaxy IVR. Mass: 3,668 kg (8,086 lb). Class: Communications. Spacecraft: HS 601. Manufacturer: Hughes Space and Communications, El Segundo. Agency: Panamsat. Perigee: 35,779 km (22,231 mi). Apogee: 35,793 km (22,240 mi). Inclination: 0.00 deg. COSPAR: 2000-020A. USAF Sat Cat: 26298. Galaxy 4R carried 28 Ku-band and 28 C-band transponders. After insertion in a standard 219 x 32007
km x 7.0 deg geostationary transfer orbit, Galaxy 4R's R-4D apogee engine raised orbit to 35765 x 35792 km x 0.1 deg by April 27 and was over 67 deg W by late April. Final destination was 99 deg W. The Galaxy satellites provide US domestic telecommunications services. 4R replaces the original Galaxy 4H which failed in May 1998, putting pagers out of action across the USA. Stationed at 99 deg W. Positioned in geosynchronous orbit at 73 deg W in 2000. As of 5 September 2001 located at 98.99 deg W drifting at 0.016 deg W per day. As of 2007 Mar 11 located at 76.88W drifting at 0.001E degrees per day.
2001 - 18:40 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-100. -
STS-100 Nation: USA. Program: ISS. Payload: Endeavour F16 / Raffaello, Canadarm-2. Mass: 103,506 kg (228,191 lb). Class: Manned. Type: Spaceplane. Spacecraft: Endeavour. Manufacturer: Boeing. Agency: NASA JSC. Perigee: 377 km (234 mi). Apogee: 394 km (244 mi). Inclination: 51.60 deg. COSPAR: 2001-016A. USAF Sat Cat: 26747. Duration: 11.90 days. Decay Date: 2001-05-01. Crew: Rominger, Ashby, Hadfield, Phillips, Parazynski, Guidoni, Lonchakov. Flight: STS-100. Space Shuttle OV-105 Endeavour was launched on mission STS-100 to carry out International Space Station Flight 6A continued the outfitting of the Station. The crew of four Americans, one Russian, one Canadian and one Italian were to install an 18 meter, 1,700 kg Canadian robotic arm named Canadarm-2 on the ISS, and to transport an Italian cargo container, Raffaello, which delivered 4,500 kg of supplies and equipment to the station. Total payload of 13,744 kg consisted of: - Bay 1-2: Orbiter Docking System, External Airlock, 3 EMU spacesuits - 2160 kg including 360 kg for the 3 suits
- Bay 3 Starboard: Adapter Beam with DCSU switching unit - 180kg
- Bay 5: Spacelab Pallet with Canadarm-2 SSRMS (Space Station Remote Manipulator System, 1800 kg mass), LDA, and 56 kg UHF antenna - 3256 kg
- Bay 6 Port: Adapter Beam with IMAX Camera - 238 kg
- Bay 8-12: Rafaello Module (MPLM-2) with MPLM racks and 3400 kg cargo - 7500 kg
- Sill: Canadarm RMS 303 - 410 kg
Endeavour reached an 80 x 317 km orbit at 1849 GMT; at 1924 GMT the OMS engines fired to raise perigee. After a series of rendezvous burns, the spaceship docked with the PMA-2 port on the ISS at 1359 GMT on April 21.On 23 April the SSRMS station manipulator was unberthed from the SLP Spacelab pallet at 1114 GMT and latched on to the PDGF fixture on the Destiny ISS module at 1416 GMT. This was followed at 1458 GMT with the MPLM-2 Raffaello module being moved from Endeavour's payload bay by the Shuttle's RMS and berthed to the nadir port on the ISS Unity module at 1600 GMT. Over the next few days, the cargo racks on the MPLM were transferred to Destiny. Raffaello was then unberthed from Unity at 2003 GMT on April 27 and reberthed in the rear of Endeavour's bay for return to earth at 2059 GMT. Undocking of Endeavour was delayed by a series of computer problems at the Station. Failures in the Station's command and control computers left only one of the three computers operating. They were all restarted by April 29, and the Shuttle RMS grappled the Spacelab pallet at 2044 GMT . The station's Canadarm-2 released it at 2106 GMT, and the RMS berthed the pallet back in the Shuttle cargo bay. Endeavour undocked from the Station at 1734 GMT on April 29. The weather in Florida was bad at the planned May 1 landing time, so Endeavour landed in California. The deorbit burn was at 1502 GMT on May 1, with landing at 1610:42 GMT on runway 22 at Edwards. Endeavour returned to the Kennedy Space Center atop a Boeing 747 SCA aircraft on May 9.
2002 - -
Air Force Space Command became a separate four-star Air Force command distinct from the US Space Command and NORAD. Nation: USA.
2002 -
2004 - 03:19 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz FG. LV Configuration: Soyuz-FG Zh15000-009. -
Soyuz TMA-4 Nation: Russia. Program: ISS. Payload: Soyuz TMA s/n 214. Mass: 7,250 kg (15,980 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz TMA. Manufacturer: RKK Energia. Agency: Rosaviakosmos. Perigee: 359 km (223 mi). Apogee: 367 km (228 mi). Inclination: 51.60 deg. Period: 91.80 min. COSPAR: 2004-013A. USAF Sat Cat: 28228. Duration: 187.89 days. Decay Date: 2004-10-24. Crew: Fincke, Padalka, Kuipers. Flight: ISS EO-8, ISS EO-9, ISS Delta. Soyuz TMA-4 was ISS transport mission ISS 8S and delivered the EO-9 caretaker crew of Gennadiy Padalka and Michael Fincke, together with the ESA/Netherlands Delta mission crewmember Andre Kuipers, to the Space Station. Soyuz TMA-4 docked with the nadir port on Zarya at 05:01 GMT on April 21 and the hatches to the ISS were opened at 06:30 GMT. Another gyro on the station had shut down prior to the docking and possibly would require a maintenance spacewalk to replace its failed electronics. After Soyuz TMA-5 docked with the ISS on October 16, the EO-9 crew handed activities over to the EO-10 crew.
2008 - 08:29 GMT -
Born on this day in:
Died on this day in: - 1990 - Vladislav Ivanovich Gulyayev
. Russian Engineer Cosmonaut. Cause of Death: Heart attack.
- 2006 - Albert Scott Crossfield. Hispanic American Pilot Test Pilot. Cause of Death: Crashed private light aircraft in bad weather near Ellijay, Georgia.
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