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On April 9 in Space History
1940 April 9 - .
- Hitler invades Norway, Denmark - .
Nation: Germany.
1940 April 9 - .
- Birth of Vasily Dmitriyevich Shcheglov - .
Nation: Russia,
Ukraine.
Related Persons: Shcheglov.
Russian pilot cosmonaut, 1965-1972. Graduated from Yeisk Higher Military Pilot School, 1963 Cosmonaut training November 1965 - December 1967. Withdrawn from cosmonaut team for medical reasons. Died of lung cancer..
1947 April 9 - .
00:10 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC33.
Launch Vehicle:
V-2.
- Solar ultraviolet / chemical release mission - .
Nation: USA.
Agency: APL,
US Army.
Apogee: 103 km (64 mi). Launched 17:13 local time. Reached 102.4 km. Carried cosmic and solar radiation, photo experiments for Applied Physics Lab, John Hopkins University..
1948 April 9 - .
- XS-1 Flight 85 - .
Crew: Lundquist.
Payload: XS-1 # 1 flight 49. Nation: USA.
Related Persons: Lundquist.
Class: Manned.
Type: Manned rocketplane. Spacecraft: XS-1.
AF flight 27. Powered pilot-check flight..
1948 April 9 - .
- XS-1 Flight 84 - .
Crew: Lilly.
Payload: XS-1 # 2 flight 36. Nation: USA.
Related Persons: Lilly.
Class: Manned.
Type: Manned rocketplane. Spacecraft: XS-1.
NACA flight 16. Stability and loads investigation. Mach 0.89..
1949 April 9 - .
LV Family:
Groettrup.
Launch Vehicle:
G-4.
- Ustinov instructs German rocket engineers to design '3000/3000' missile. - .
Nation: Russia.
Related Persons: Ustinov.
Ustinov's requirement was to deliver a 3000 kg nuclear warhead over a 3000 km range (eg to reach the United Kingdom)..
1950 April 9 - .
- Birth of Kenneth Dale 'Taco' Cockrell - .
Nation: USA.
Related Persons: Cockrell.
American test pilot astronaut 1990-2006. 5 spaceflights, 64.5 days in space. Flew to orbit on STS-56 (1993), STS-69, STS-80, STS-98, STS-111..
1954 April 9 - .
LV Family:
Atlas,
Thor.
- Ballistic missiles to move forward with all practicable speed. - .
In a memorandum to Secretary of the Air Force Harold E. Talbott, Deputy Secretary of Defense Roger M. Keyes stressed that the plans for the ballistic missile program "be formulated with a thoroughly realistic appraisal of the capabilities of our contractors to meet their commitments." He then emphasized that the program was to move forward "with all practicable speed."
1954 April 9 - .
21:12 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC35.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee RTV-N-10.
- Mass spectrometer Aeronomy mission - .
Nation: USA.
Agency: NRL.
Apogee: 143 km (88 mi). Gas composition research. Launched at 1412 local time. Reached 143 km..
1955 April 9 - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar V-2.
LV Family:
V-2.
Launch Vehicle:
R-1 8A11.
1957 April 9 - .
15:19 GMT - .
Launch Site:
Holloman.
Launch Complex:
Holloman A.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee AJ10-25.
- Meteorites mission - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 61 km (37 mi). Micrometeorites research. Launched at 0819 local time. Reached 61 km..
1958 April 9 - .
LV Family:
Minuteman.
- STL responsible for the Minuteman program. - .
The Space Technology Laboratories (STL) was made responsible for SE/TD of the Minuteman program..
1959 April 9 - .
- First group of US astronauts announced - .
Nation: USA.
Related Persons: Glennan.
Spacecraft: Mercury.
At a press conference in Washington, D.C., NASA Administrator T. Keith Glennan announced the seven pilots had been selected for the Mercury program..
1959 April 9 - .
Launch Site:
Kapustin Yar.
LV Family:
R-5.
Launch Vehicle:
R-5M.
- Zvezda - .
Nation: Russia.
Agency: RVSN.
Apogee: 500 km (310 mi).
1961 April 9 - .
09:16 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC51.
LV Family:
R-9.
Launch Vehicle:
R-9A.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,160 km (720 mi). The R-9 launch went normally, from the launch pad adjacent to that from which Yuri Gagarin would be launched three days later, in view of the cosmonauts..
1962 April 9 - .
15:04 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Midas 5 - .
Payload: Midas / Agena TV 1203. Mass: 1,860 kg (4,100 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
USAF Sat Cat: 271 . COSPAR: 1962-Kappa-1. Apogee: 3,405 km (2,115 mi). Perigee: 2,784 km (1,729 mi). Inclination: 86.70 deg. Period: 152.90 min. Missile Defense Alarm System..
- West Ford Drag - .
Payload: West Ford Drag Experiment. Nation: USA.
Agency: USAF.
Spacecraft: WestFord Needles.
Decay Date: 1962-05-04 . USAF Sat Cat: 272 . COSPAR: 1962-Kappa-2. Apogee: 2,729 km (1,695 mi). Perigee: 99 km (61 mi). Inclination: 86.64 deg. Period: 114.09 min.
1962 April 9 - .
20:50 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC11.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
FAILURE: Failure.
Failed Stage: 1.
- Research and development launch - .
Nation: USA.
Agency: USAF.
1963 April 9 - .
- Vostok proposed as the first 'space trainer'. - .
Nation: Russia.
Related Persons: Keldysh,
Korolev.
Spacecraft: Vostok.
In a meeting between the VVS and OKB-1 engineers, Korolev and Keldysh push for acceptance by the military and use of Vostok as the first 'space trainer'. Cosmonauts would train for spaceflight on Vostok missions before being assigned to operational flights aboard Soyuz.. This was consistent with aircraft practice (e.g. where the first effective jet fighter, the MiG-15, was converted to the MiG-15UTI and became the standard jet trainer for the VVS). It also envisioned a future where operational Vostok and Soyuz spacecraft would be mass-produced by the military and flown as regularly as fighter aircraft.
1963 April 9 - .
- Birth of Timothy Lennart Kopra - .
Nation: USA.
Related Persons: Kopra.
American engineer mission specialist astronaut 2000-2018. 2 spaceflights, 244.0 days in space. Flew to orbit on STS-127 (2009), Soyuz TMA-19M..
1963 April 9 - .
20:28 GMT - .
Launch Site:
Wallops Island.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- D-region Ionosphere mission - .
Nation: USA.
Agency: NASA.
Apogee: 163 km (101 mi).
1964 April 9 - .
14:22 GMT - .
Launch Site:
Sonmiani.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- Rehbar 4? (Na) Aeronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 160 km (90 mi).
1964 April 9 - .
20:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC15.
LV Family:
Titan.
Launch Vehicle:
Titan II.
- Research and development / Pod RVIP test / plume study mission - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
The 23d, and last, Titan II research and development missile (N-3A) to be launched down the Atlantic range completed a success ful flight. With the 10 test flights from Vandenberg, a total of 33 Titan II (XLGM-25C) R&D flights had been completed since 16 March 1962 - 27 successes and only six failures. This Air Force conducted test program contributed significantly to the development of the Gemini launch vehicle; the Gemini malfunction detection system was tested on five flights, Gemini guidance components on three, and the longitudinal oscillation fix on four. In addition to flight testing these (and other) critical components, these flights also enhanced confidence in the use of the Titan II as a launch vehicle. Thirty-two Titan II test flights were analyzed to determine whether any characteristic of the flight would have demanded a Gemini abort; 22 were adjudged successful from the standpoint of a Gemini mission, nine would have required Gemini to abort, and one resulted in a prelaunch shutdown.
1965 April 9 - .
- Manned space flight control transferred to Houston - .
Nation: USA.
Related Persons: Mueller.
Program: Apollo.
George E. Mueller, Associate Administrator for Manned Space Flight, announced the transfer of control over manned space flights from Cape Kennedy, Fla., to Houston, Texas. MSC's Mission Control Center would direct the flights from end of liftoff through recovery.
1965 April 9 - .
01:01 GMT - .
Launch Site:
Woomera.
Launch Complex:
Woomera LA2.
Launch Pad: LA2 SL.
Launch Vehicle:
Skylark.
1965 April 9 - .
18:10 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC18A.
Launch Pad: LC18A.
LV Family:
Scout.
Launch Vehicle:
Blue Scout Jr.
- OAR 22-9 / AFWL-14 Magnetosphere mission - .
Nation: USA.
Agency: USAF.
Apogee: 25,422 km (15,796 mi).
1965 April 9 - .
19:18 GMT - .
Launch Pad: Pacific Ocean, 44.3 S x 77.7 W.
Launch Platform: CVE-25.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- Ionosphere mission - .
Nation: USA.
Agency: NASA.
Apogee: 191 km (118 mi). Launched at 1965 Croatan MRF Expedition LP36 - - Latitude: 44.25 S - Longitude: 77.67 W..
1965 April 9 - .
20:26 GMT - .
Launch Pad: Pacific Ocean, 44.4 S x 77.8 W.
Launch Platform: CVE-25.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- UM Pitot 12 Aeronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 147 km (91 mi). Launched at 1965 Croatan MRF Expedition LP37 - - Latitude: 44.38 S - Longitude: 77.78 W..
1966 April 9 - .
- Cost and schedule estimates for MSFC to integrate the ATM with the LEM. - .
Nation: USA.
Spacecraft Bus: Skylab.
Spacecraft: Apollo ATM,
Skylab.
In response to a request from Deputy Administrator Robert C. Seamans, Jr., Saturn/Apollo Applications Deputy Director John H. Disher asked Jerry McCall, MSFC' Deputy Director for Research and Development Operations, to prepare cost and schedule estimates for 'MSFC to integrate the ATM with the LEM. This request stemmed from a desire by the Office of Space Science and Applications (OSSA) to acquire ATM experiment data during upcoming periods of maximum solar activity. Disher listed guidelines for the MSFC estimates: OSSA-desired flight dates were April 1968, February 1969, and February 1970. Goddard Space Flight Center would be responsible for development of experiments aboard the ATM, as well as for the mounting structure and thermal provisions. MSFC would be responsible for development of modification kits to convert all Apollo lunar-landing-configured LEM to an AAP laboratory configuration (including provisions for reuse after three to six mouths storage in orbit); for development of interface modification kits needed to integrate the ATM and its experiments with the AAP LEM laboratory; and for installation of the modification kits and the ATM system in the LEM at KSC prior to checkout and launch. In addition, Disher told McCall that MSFC should examine two approaches to ATM LEM integration: (1) gimbal mounted and (2) hard mounted with provisions for momentum transfer for fine pointing control.
1967 April 9 - .
01:00 GMT - .
Launch Site:
Kiruna.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- DLR K-NA-3 Aurora / barium release mission - .
Nation: USA.
Agency: NASA.
Apogee: 242 km (150 mi).
1968 April 9 - .
Launch Site:
Biscarosse.
Launch Complex:
Biscarosse BLB.
LV Family:
MSBS.
Launch Vehicle:
SSBS S01.
- S01V-4 test - .
Nation: France.
Agency: DMA.
Apogee: 500 km (310 mi).
1968 April 9 - .
Launch Site:
Kourou.
Launch Complex:
Kourou ALFS.
LV Family:
Veronique.
Launch Vehicle:
Veronique AGI.
- FU-184 Sea recovery test - .
Nation: France.
Agency: CNES.
Apogee: 114 km (70 mi). FU184 Technology (sea recovery) mission..
1968 April 9 - .
11:26 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC133/1.
LV Family:
R-12.
Launch Vehicle:
Kosmos 11K63.
- Cosmos 211 - .
Payload: DS-P1-Yu s/n 13. Mass: 250 kg (550 lb). Nation: Russia.
Agency: MO.
Program: DS.
Class: Military.
Type: Military target satellite. Spacecraft Bus: DS.
Spacecraft: DS-P1-Yu.
Completed Operations Date: 1968-04-13 . Decay Date: 1968-11-10 . USAF Sat Cat: 3181 . COSPAR: 1968-028A. Apogee: 1,532 km (951 mi). Perigee: 199 km (123 mi). Inclination: 81.90 deg. Period: 102.30 min. Development of systems for air defence and the control of outer space..
1968 April 9 - .
21:26 GMT - .
Launch Site:
Wallops Island.
LV Family:
Honest John.
Launch Vehicle:
Javelin.
- Extreme ultraviolet Dayglow Aeronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 856 km (531 mi).
1969 April 9 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC25C.
LV Family:
Polaris.
Launch Vehicle:
Poseidon C3.
- Test mission - .
Nation: USA.
Agency: USN.
Apogee: 500 km (310 mi).
1969 April 9 - .
09:33 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar V-2.
Launch Vehicle:
MR-12.
- Aeronomy mission - .
Nation: Russia.
Agency: AN.
Apogee: 170 km (100 mi).
1969 April 9 - .
13:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 278 - .
Payload: Zenit-2 11F61 s/n 78. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1969-04-17 . USAF Sat Cat: 3883 . COSPAR: 1969-034A. Apogee: 310 km (190 mi). Perigee: 198 km (123 mi). Inclination: 65.40 deg. Period: 89.60 min. Area survey photo reconnaissance satellite..
1969 April 9 - .
20:38 GMT - .
Launch Site:
Andoya.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- Ferdinand 20 Aeronomy / ionosphere / plasma mission - .
Nation: Norway.
Agency: NTNF.
Apogee: 139 km (86 mi).
1970 April 9 - .
- State Commission is held to review issues of the Soyuz 9 flight. - .
Nation: Russia.
Related Persons: Mishin.
Program: Soyuz.
Flight: Soyuz 9.
All is ready for a flight in April, but the Communist Party resolution says the flight has to wait for May. The Soyuz ECS is designed to only operate for five days, but will have to operate 3 to 4 times longer for this mission. Various problems are identified and reviewed. Mishin wants to accept a carbon dioxide level in the cabin atmosphere double the percentage considered acceptable earlier. Plans are made for a quick flight of the crew after the long duration mission to Moscow for extensive physical examinations.
1971 April 9 - .
1973 April 9 - .
Launch Site:
Baikonur.
Launch Vehicle:
UR-100N.
- Mod 2 state trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1974 April 9 - .
05:21 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Tomahawk.
Launch Vehicle:
Ute Tomahawk.
- Churchill 74 Aeronomy mission - .
Nation: USA.
Agency: USAF CRL.
Apogee: 169 km (105 mi).
1975 April 9 - .
23:58 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 1410.
- Geos 3 - .
Payload: GEOS C. Mass: 341 kg (751 lb). Nation: USA.
Agency: NASA Wallops.
Class: Astronomy.
Type: Solar satellite. Spacecraft: Geos.
USAF Sat Cat: 7734 . COSPAR: 1975-027A. Apogee: 848 km (526 mi). Perigee: 817 km (507 mi). Inclination: 115.00 deg. Period: 101.60 min.
Geodynamics Experimental Ocean Satellite. The mission of GEOS 3 (Geodynamics Experimental Ocean Satellite) was to provide the stepping stone between the National Geodetic Satellite Program (NGSP) and the Earth and Ocean Physics Application Program. It provided data to refine the geodetic and geophysical results of the NGSP and served as a test for new systems. A major achievment was the flight of a radar altimeter. Further mission objectives: intercomparison of tracking systems, investigation of solid-earth dynamic phenomena through precision laser tracking, refinement of orbit determination techniques, determination of interdatum ties and gravity models, and support of the calibration and position determination of NASA Spaceflight Tracking and Data Network (STDN) S-band tracking stations.
1976 April 9 - .
- Birth of Serena Maria Auñón - .
Nation: USA.
Related Persons: Aunon.
American physician mission specialist astronaut, 2009-on. 1 spaceflight, 196.7 days in space. Flew to orbit on Soyuz MS-09 (2018)..
1976 April 9 - .
08:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 813 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1976-04-21 . USAF Sat Cat: 8801 . COSPAR: 1976-033A. Apogee: 236 km (146 mi). Perigee: 209 km (129 mi). Inclination: 81.30 deg. Period: 88.90 min. Area survey photo reconnaissance satellite; returned film capsule..
1978 April 9 - .
- A fire occurred in the FLTSATCOM assembly area of the TRW facility in Redondo Beach, California. - .
Spacecraft: FLTSATCOM.
Many pieces of FLTSATCOM hardware were damaged by soot and smoke, and some suffered water damage. The fire caused a two-month delay in the testing of the second FLTSATCOM satellite and a four-month delay in the integration of the third satellite..
1978 April 9 - .
04:50 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant 8B.
- E / / B Aurora active mission - .
Nation: USA.
Agency: NASA.
Apogee: 247 km (153 mi).
1980 April 9 - .
13:38 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 35 - .
Call Sign: Dnepr (Dnieper ). Crew: Popov,
Ryumin.
Backup Crew: Andreyev,
Zudov.
Payload: Soyuz 7K-T s/n 51. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Related Persons: Andreyev,
Popov,
Ryumin,
Zudov.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 35.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 55.06 days. Decay Date: 1980-06-03 . USAF Sat Cat: 11753 . COSPAR: 1980-027A. Apogee: 247 km (153 mi). Perigee: 197 km (122 mi). Inclination: 51.60 deg. Period: 88.90 min. Manned two crew. Docked with Salyut 6. Carried crew comprising L I Popov and V V Ryumin to the Salyut-6 station to carry out scientific and technical research and experiments..
1981 April 9 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1263 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
USAF Sat Cat: 12388 . COSPAR: 1981-033A. Apogee: 1,684 km (1,046 mi). Perigee: 387 km (240 mi). Inclination: 83.00 deg. Period: 105.90 min. Radar calibration mission..
1982 April 9 - .
08:00 GMT - .
Launch Site:
Sea Launch Area.
Launch Pad: UNKO.
Launch Platform: MUSSON.
Launch Vehicle:
MMR-06.
- Aeronomy mission - .
Nation: Russia.
Agency: GMS.
Apogee: 58 km (36 mi).
1983 April 9 - .
- STS-6 - Wakeup Song: Ode to the Lions - .
Flight: STS-6.
"Ode to the Lions" as rendered by Rusty Gordon. This is a Penn State song referring to the Nittany Lions, of Penn State University which is Paul Weitz alma mater. He earned his Bachelor in Aeronautical Engineering at Penn State in 1954..
1983 April 9 - .
14:30 GMT - .
Launch Site:
Wallops Island.
Launch Vehicle:
Super Loki.
- Test / aeronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 109 km (67 mi).
1983 April 9 - .
1984 April 9 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 645.
LV Family:
Polaris.
Launch Vehicle:
Poseidon C3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 500 km (310 mi).
1984 April 9 - .
05:16 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 645.
LV Family:
Polaris.
Launch Vehicle:
Poseidon C3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 500 km (310 mi).
1985 April 9 - .
17:30 GMT - .
Launch Site:
Primrose Lake.
LV Family:
Deacon.
Launch Vehicle:
Rocketsonde.
- Arcasonde - .
Nation: USA.
Agency: MRN.
Apogee: 66 km (41 mi).
1986 April 9 - .
Launch Site:
Balasore.
LV Family:
RH.
Launch Vehicle:
RH-200.
- Nation: India.
Agency: ISRO.
Apogee: 60 km (37 mi).
1986 April 9 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1739 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1986-06-07 . USAF Sat Cat: 16677 . COSPAR: 1986-028A. Apogee: 326 km (202 mi). Perigee: 171 km (106 mi). Inclination: 64.90 deg. Period: 89.50 min. 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 April 9 - .
11:44 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1835 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 56.00 days. Decay Date: 1987-06-04 . USAF Sat Cat: 17849 . COSPAR: 1987-032A. Apogee: 343 km (213 mi). Perigee: 170 km (100 mi). Inclination: 64.80 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1988 April 9 - .
00:40 GMT - .
Launch Site:
Kiruna.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant VB.
- ERRRIS I Ionosphere mission - .
Nation: USA.
Agency: NASA.
Apogee: 128 km (79 mi).
1989 April 9 - .
04:37 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant XB.
- Barium release + Plasma mission - .
Nation: USA.
Agency: NASA.
Apogee: 700 km (430 mi).
1990 April 9 - .
08:50 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC36.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant IX.
- Astronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 300 km (180 mi).
1991 April 9 - .
- STS-37 - Wakeup Song: 10,000 Men of Harvard Want Victory Today - .
Flight: STS-37.
"10,000 Men of Harvard Want Victory Today" sung by Harvard Glee Club, in honor of Jay Apt, a Harvard graduate. About five minutes after the wake up call, Apt played a recorded Scottish tune from Atlantis in honor of the highest and fastest Highlanders, Ross and Cameron.
1991 April 9 - .
18:50 GMT - .
Launch Site:
Kiruna.
Launch Complex:
Kiruna S.
LV Family:
Skylark.
Launch Vehicle:
Skylark 7.
- SISSI 4 Aeronomy mission - .
Nation: Germany.
Agency: DLR.
Apogee: 245 km (152 mi).
1992 April 9 - .
10:40 GMT - .
Launch Site:
Kiruna.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant 9BM1.
- MASER 5 Microgravity mission - .
Nation: Europe.
Agency: SSC.
Apogee: 317 km (196 mi).
1994 April 9 - .
11:05 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39A.
Launch Platform: MLP2.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- MAPS - .
Nation: USA.
Agency: NASA.
Program: STS.
Spacecraft Bus: Shuttle Attached Payloads.
Spacecraft: MAPS.
Decay Date: 1994-04-20 . USAF Sat Cat: 23042 . COSPAR: 1994-020xx. Apogee: 211 km (131 mi). Perigee: 202 km (125 mi). Inclination: 57.00 deg. Period: 88.60 min. Air pollution experiment carried in shuttle bay..
- SRL-1 - .
Payload: SRL PLT. Nation: USA.
Agency: NASA.
Program: STS.
Spacecraft Bus: Shuttle Attached Payloads.
Spacecraft: SLP.
Decay Date: 1994-04-20 . USAF Sat Cat: 23042 . COSPAR: 1994-020xx. Apogee: 211 km (131 mi). Perigee: 202 km (125 mi). Inclination: 57.00 deg. Period: 88.60 min.
1995 April 9 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 734.
LV Family:
Trident.
Launch Vehicle:
Trident D-5.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1995 April 9 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 734.
LV Family:
Trident.
Launch Vehicle:
Trident D-5.
- Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1995 April 9 - .
19:34 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
1997 April 9 - .
08:58 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2340 - .
Payload: Oko #77. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MO.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 24761 . COSPAR: 1997-015A. Apogee: 37,201 km (23,115 mi). Perigee: 3,164 km (1,966 mi). Inclination: 65.20 deg. Period: 718.00 min. Covered Oko constellation planes 8/9 - 217 degree longitude of ascending node..
1999 April 9 - .
17:01 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 402B/IUS.
FAILURE: IUS first and second stages failed to separate..
Failed Stage: U.
- USA 142 - .
Payload: DSP-1 Block 18 F19. Mass: 2,380 kg (5,240 lb). Nation: USA.
Agency: USAF.
Manufacturer: TRW.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
USAF Sat Cat: 25669 . COSPAR: 1999-017A. Apogee: 35,800 km (22,200 mi). Perigee: 720 km (440 mi). Inclination: 28.00 deg.
The Titan 4B placed the IUS upper stages and DSP-1 Block 14 ballistic missile launch detection satellite. payload into a 188 km x 718 km x 28.6 deg parking orbit. The first stage of the IUS burned at 18:14 GMT and put the second stage and payload into a geosynchronous transfer orbit. The IUS second stage fired at 23:34 GMT in order to place the spacecraft in geosynchronous orbit. However, at least one connector remained attached between the stages, and the second stage motor nozzle did not extend properly. When the stage fired, the vehicle tumbled wildly during the burn. Separation of the DSP was achieved. Although it could not perform its primary mission, it did provide a good test case in that the effects of radiation on its systems could be monitored as they underwent twice-daily passages of the Van Allen Radiation Belts. However after some weeks the hydrazine propellant aboard the satellite vented into space due to a broken fuel line. It was believed this had been induced by the wild ride aboard the IUS-2 stage.
2002 April 9 - .
- STS-110 Mission Status Report #03 - .
Nation: USA.
Related Persons: Bloomfield,
Bursch,
Frick,
Morin,
Ochoa,
Onufrienko,
Ross,
Smith, Steven,
Walheim,
Walz.
Program: ISS.
Flight: STS-108 ISS EO-4,
STS-110.
Working quietly but efficiently, Atlantis' astronauts completed preparations today for Wednesday's scheduled docking to the International Space Station, testing spacesuits, rendezvous tools and the shuttle's robotic arm..
Additional Details: here....
2002 April 9 - .
- STS-110 - Wakeup Song: The Best Years of Our Lives - .
Flight: STS-110.
"The Best Years of Our Lives" by the Baha Men..
2003 April 9 - .
22:52 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA3.
LV Family:
Ariane 5.
Launch Vehicle:
Ariane 5G.
- Insat 3A - .
Mass: 2,958 kg (6,521 lb). Nation: India.
Agency: ISRO.
Program: Insat.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: Insat 2.
Spacecraft: Insat 3.
USAF Sat Cat: 27714 . COSPAR: 2003-013A. Apogee: 35,802 km (22,246 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Return to flight of Ariane 5G after grounded following Ariane 5EC-A failure. Launch delayed from February 24, April 8, 2003. Satellite also had meteorological instruments. As of 2007 Mar 10 located at 93.48E drifting at 0.009W degrees per day..
- Galaxy 12 - .
Mass: 1,792 kg (3,950 lb). Nation: USA.
Agency: PanAmSat.
Manufacturer: OSC.
Program: Galaxy.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: Star bus.
USAF Sat Cat: 27715 . COSPAR: 2003-013B. Apogee: 35,791 km (22,239 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.10 deg. Period: 1,436.10 min. As of 2007 Mar 11 located at 125.09W drifting at 0.001W degrees per day..
2004 April 9 - .
- International Space Station Status Report #04-18 - .
Nation: USA.
Related Persons: Fincke,
Foale,
Kaleri,
Kuipers,
Padalka.
Program: ISS.
Flight: Soyuz TMA-3.
Three weeks remain in the six-month voyage aboard the International Space Station for Commander Mike Foale and Flight Engineer Alexander Kaleri as the Expedition 8 crew prepares to return home later this month. Their week aboard the station focused on wrapping up science experiments and tidying up for their replacement crew, which is in Russia for launch preparations. Additional Details: here....
2007 April 9 - .
22:54 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/39.
LV Family:
Proton.
Launch Vehicle:
Proton-M/Briz-M.
- Anik F3 - .
Payload: Eurostar 3000S. Mass: 4,634 kg (10,216 lb). Nation: Canada.
Agency: Telesat.
Manufacturer: Friedrichshafen.
Program: Anik.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: Eurostar 3000.
USAF Sat Cat: 31102 . COSPAR: 2007-009A. Apogee: 35,795 km (22,241 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.00 deg. Period: 1,436.20 min. Communications satellite with C, Ku and Ka band transponders..
2008 April 9 - .
- ISS On-Orbit Status 04/09/08 - .
Nation: USA.
Related Persons: Kononenko,
Malenchenko,
Reisman,
Volkov, Sergey,
Whitson,
Yi Soyeon.
Program: ISS.
Flight: Soyuz TMA-11,
Soyuz TMA-12,
STS-123 ISS EO-16,
STS-124.
Soyuz TMA-12/16S, with Expedition 17 crewmembers CDR Sergei Alexandrovich Volkov (CDR) and Oleg Dmitrievich Kononenko (FE-1), plus Korean SFP (Spaceflight Participant) So-Yeon Yi, 14th Visiting Crewmember (VC) to spend time on the station, continues to catch up with the ISS for the docking tomorrow morning at ~9:02am EDT. Additional Details: here....
2010 April 9 - .
- STS-131 - Wakeup Song: We Weren't Born to Follow - .
Flight: STS-131.
"We Weren't Born to Follow" by Bon Jovi, played for Mission Specialist Rick Mastracchio..
2010 April 9 - .
- EVA STS-131-1 - .
Crew: Anderson, Clayton,
Mastracchio.
EVA Duration: 0.27 days. Nation: USA.
Program: ISS.
Flight: Soyuz TMA-17,
Soyuz TMA-18,
STS-131.
Relocated a new ammonia tank from the Shuttle's payload bay to a temporary stowage location and disconnected the fluid lines to the old ammonia tank on the S1 truss. Retrieved a Japanese seed experiment from the exterior of the Kibo laboratory for return .
2011 April 9 - .
20:47 GMT - .
Launch Site:
Xichang.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 3A.
- Beidou IGS 3 - .
Payload: Beidou DW8. Mass: 2,600 kg (5,700 lb). Nation: China.
Agency: SISE.
Class: Navigation.
Type: Navigation satellite. Spacecraft: Beidou-IGSO.
USAF Sat Cat: 37384 . COSPAR: 2011-013A. Apogee: 35,874 km (22,291 mi). Perigee: 35,696 km (22,180 mi). Inclination: 55.30 deg. Period: 1,436.00 min. Third satellite placed in the Beidou-2 inclined geosynchronous orbit constellation; placed in Plane 1 at 118 deg E. This completed population of the first plane of the IGSO component..
2014 April 9 - .
15:26 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
2014 April 9 - .
19:06 GMT - .
Launch Site:
Palmachim.
Launch Pad: xxx.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq-10 - .
Mass: 260 kg (570 lb). Nation: Israel.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Tecsar.
USAF Sat Cat: 39650 . COSPAR: 2014-019A. Apogee: 598 km (371 mi). Perigee: 388 km (241 mi). Inclination: 140.94 deg. Period: 94.48 min. Reportedly carried a radar imaging (SAR) payload..
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