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On July 10 in Space History
1900 July 10 - .
- Birth of Theodore Buchhold - .
Nation: Germany,
USA.
Related Persons: Buchhold.
German professor. Member of the German Rocket Team in the United States after WW2. German expert in guided missiles during WW2. As of January 1947, working at Fort Bliss, Texas. Died at Wiesbaden, Germany..
1917 July 10 - .
- Birth of Robert W Kamm - .
Nation: USA.
Related Persons: Kamm.
American aerodynamicist, at NASA 1939-1946, 1959-1968. Served in NASA California management positions..
1942 July 10 - .
- Birth of Pyotr Ilyich Klimuk - .
Nation: Belarus.
Related Persons: Klimuk.
Belarusian pilot cosmonaut 1965-1982. 3 spaceflights, 78.8 days in space. Flew to orbit on Soyuz 13 (1973), Soyuz 18, Soyuz 30..
1947 July 10 - .
19:18 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC33.
Launch Vehicle:
V-2.
FAILURE: Failure.
- Aeronomy mission - .
Nation: USA.
Agency: NRL,
US Army.
Apogee: 16 km (9 mi). Launched 12:18 local time. Reached 16.1 km. Carried cosmic radiation, pressure, temperature, ionosphere, biological (Harvard) experiments for Naval Research Lab..
1950 July 10 - .
Launch Vehicle:
Redstone.
1950 July 10 - .
- Birth of Christopher John Nicholas Holmes - .
Nation: UK.
Related Persons: Holmes.
British physicist payload specialist astronaut, 1984-1986. Bachelor of Science in physics from the Queen Mary College, London, 1972. Physicist. Selected in 1984 for the British Skynet-Program. British National Space Center, London..
1951 July 10 - .
Launch Vehicle:
Redstone.
- Hermes work transferred to Redstone arsenal. - .
Nation: USA.
Related Persons: von Braun.
The Office, Chief of Ordnance formally transferred the responsibility for conducting the research and development phase of the HERMES Cl project to Redstone Arsenal.
1958 July 10 - .
LV Family:
Atlas.
- Advanced Research Projects Agency questions - .
Spacecraft: Man-In-Space-Soonest.
The Advanced Research Projects Agency addressed two questions to the research and development command: Would the Air Force accept a 110 nautical mile orbit instead of 150 nautical miles for the manned space flight? What degree of program accomplishment could be obtained with a fiscal 1959 program of $50 million based on an Atlas-117L second stage? (Chronological "Space Hi't, 1958.)
1958 July 10 - .
02:30 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17A.
LV Family:
Thor.
Launch Vehicle:
Thor Able.
- Able RTV re-entry vehicle test flight - .
Nation: USA.
Agency: USAF.
Apogee: 1,600 km (900 mi).
Mouse 'Mia II' reached 1600 km altitude, flew 9600 km range, but re-entry vehicle not recovered. The second Air Force Thor/Able reentry (nose cone) test vehicle, testing a GE ablation-type nose cone, was launched from Cape Canaveral on a 6,000-mile flight down the Atlantic Missile Range. This was the first U.S. reentry vehicle to make a full-range ICBM flight and reentry.
1958 July 10 - .
07:42 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Vehicle:
R-7.
FAILURE: Failure.
- B1-14 (II-5)/Blok E test - .
Nation: Russia.
Agency: MVS.
Apogee: 0 km (0 mi).
1959 July 10 - .
01:01 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC26B.
LV Family:
Jupiter.
Launch Vehicle:
Jupiter IRBM.
- Research and development test / ionosphere mission - .
Nation: USA.
Agency: NASA Huntsville,
USAF.
Apogee: 500 km (310 mi).
Fired from AMR at 2001 hours EST to test missile accuracy. All primary and secondary missions were successfully accomplished and impact was well within 1 nm of the pre-selected point, approximately 1,302 nm downrange -- a miss distance of only 0.48 nm short and 0.09 nm to the right.
1959 July 10 - .
04:47 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar V-2.
LV Family:
V-2.
Launch Vehicle:
R-2A.
- Solar ultraviolet / biology mission - .
Nation: Russia.
Agency: MVS.
Apogee: 100 km (60 mi).
1962 July 10 - .
- First Apollo mockup inspection - .
Nation: USA.
Related Persons: Gilruth,
Grissom.
Program: Apollo.
The first Apollo spacecraft mockup inspection was held at NAA's Space and Information Systems Division. In attendance were Robert R. Gilruth, Director, MSC; Charles W. Frick, Apollo Program Manager, MSC; and Astronaut Virgil I. Grissom..
1962 July 10 - .
08:35 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
LV Family:
Thor.
Launch Vehicle:
Thor Delta.
- Telstar 1 - .
Mass: 77 kg (169 lb). Nation: USA.
Agency: ATT.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: Telstar.
USAF Sat Cat: 340 . COSPAR: 1962-A-Epsilon-1. Apogee: 5,643 km (3,506 mi). Perigee: 945 km (587 mi). Inclination: 44.80 deg. Period: 157.80 min.
A NASA Thor/Delta boosted Telstar, the first commercially developed international communications satellite, into orbit. First commercial comsat; active repeater. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).
1962 July 10 - .
15:00 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC35.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee 150.
- Radar test Technology test - .
Nation: USA.
Agency: NASA.
Apogee: 200 km (120 mi).
1963 July 10 - .
- Odintsev pressing criticism of Tereshkova - .
Nation: Russia.
Related Persons: Tereshkova.
Flight: Vostok 6.
Odintsev is still trying to formally criticise Tereshkova for her flight performance. He charges that she was drunk when she reported to the launch pad and while in orbit was insubordinate, disregarding direct orders from the Centre. Kamanin knows this to be absolutely not true. Both cosmonauts and workers at the cosmonaut training centre report that is impossible to work with Odintsev any more - they want him out.
1963 July 10 - .
- Prototype engine for the Apollo SM reaction control system - .
Nation: USA.
Program: Apollo.
Spacecraft: Apollo CSM,
CSM RCS.
The Marquardt Corporation began testing the prototype engine for the SM reaction control system. Preliminary data showed a specific impulse slightly less than 300 seconds..
1963 July 10 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
FAILURE: Shutdown of Block B strap-on engine stage 1.9 seconds after liftoff. Pad damaged..
Failed Stage: 0.
- Zenit-2 11F61 s/n 12 - .
Payload: Zenit-2 11F61 s/n 12. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Decay Date: 1963-07-10 . Area survey photo reconnaissance satellite..
1963 July 10 - .
02:46 GMT - .
Launch Site:
Wallops Island.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee 150A.
- Ionosphere mission - .
Nation: USA.
Agency: NASA.
Apogee: 204 km (126 mi).
1963 July 10 - .
17:02 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC35.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee 150.
- Extreme ultraviolet Mon / RPA Solar ultraviolet mission - .
Nation: USA.
Agency: USAF.
Apogee: 225 km (139 mi).
1964 July 10 - .
- New Space Systems Division headquarters at Los Angeles Air Force Station, California - .
Related Persons: Schriever.
In ceremonies commemorating the 10th Anniversary of the Air Force Ballistic missile program and activation of the former Western Development Division (WDD), General Bernard A. Schriever, Commander, AFSC, dedicated the new Space Systems Division headquarters and facilities at Los Angeles Air Force Station, California.
1964 July 10 - .
21:51 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8K72K.
- Elektron 3 - .
Payload: 2D s/n 3. Mass: 350 kg (770 lb). Nation: Russia.
Agency: Korolev bureau.
Program: Elektron.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: Elektron-A.
USAF Sat Cat: 829 . COSPAR: 1964-038A. Apogee: 6,302 km (3,915 mi). Perigee: 408 km (253 mi). Inclination: 60.90 deg. Period: 159.30 min. Studied inner Van Allen belt. Electron 3 and 4 launched by a single carrier rocket. Simultaneous study of the inner and outer radiation belts of the earth, cosmic rays and the upper atmosphere. .
- Elektron 4 - .
Payload: 2D s/n 4. Mass: 444 kg (978 lb). Nation: Russia.
Agency: Korolev bureau.
Program: Elektron.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: Elektron-B.
Decay Date: 1983-10-12 . USAF Sat Cat: 830 . COSPAR: 1964-038B. Apogee: 66,269 km (41,177 mi). Perigee: 447 km (277 mi). Inclination: 60.80 deg. Period: 1,313.80 min. Studied outer Van Allen belt. Electron 3 and 4 launched by a single carrier rocket. Simultaneous study of the inner and outer radiation belts of the earth, cosmic rays and the upper atmosphere. .
1964 July 10 - .
23:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1008 - .
Payload: KH-4A s/n 1008 / Agena D 1117 / OPS 3491. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-08-06 . USAF Sat Cat: 828 . COSPAR: 1964-037A. Apogee: 346 km (214 mi). Perigee: 173 km (107 mi). Inclination: 84.90 deg. Period: 89.70 min. KH-4A. Cameras operated satisfactorily, some light leaks..
1965 July 10 - .
Launch Site:
Baikonur.
Launch Vehicle:
UR-100.
FAILURE: Failure.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 0 km (0 mi).
1966 July 10 - .
- Komarov announces that USSR will beat US to moon - .
Nation: Russia.
Related Persons: Komarov.
Program: Lunar L3.
Class: Manned.
Type: Manned space station. Komarov announces in Japan that USSR would beat the US to moonlanding by one year..
1968 July 10 - .
- L3 recovery controversy. - .
Nation: Russia.
Related Persons: Grechko, Andrei,
Mishin,
Ryabikov,
Zakharov.
Program: Lunar L3.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-LOK.
Marshal Zakharov has consulted with Ryabikov at Gosplan on what commitments Grechko has made from Ministry of Defence funds for L3 recovery forces. Gosplan advised him that 800 million roubles and 21,000 staff were committed, but the justification for these amounts were not methodically developed. Mishin is now saying that hundreds, not thousands of cadres will be required, see he can set the return capsule down in within the confines of the cosmodrome.
1968 July 10 - .
Launch Site:
Bershet.
Launch Vehicle:
UR-100.
- Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1968 July 10 - .
19:49 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 231 - .
Payload: Zenit-2 11F61 s/n 64. 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: 1968-07-18 . USAF Sat Cat: 3316 . COSPAR: 1968-058A. Apogee: 311 km (193 mi). Perigee: 206 km (128 mi). Inclination: 64.90 deg. Period: 89.60 min. Area survey photo reconnaissance satellite..
1969 July 10 - .
08:07 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar V-2.
Launch Vehicle:
MR-12.
- Ionosphere mission - .
Nation: Russia.
Agency: AN.
Apogee: 162 km (100 mi).
1969 July 10 - .
09:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 289 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 5.00 days. Decay Date: 1969-07-15 . USAF Sat Cat: 4034 . COSPAR: 1969-057A. Apogee: 324 km (201 mi). Perigee: 194 km (120 mi). Inclination: 65.30 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 July 10 - .
12:31 GMT - .
Launch Site:
Ile du Levant.
LV Family:
Belier.
Launch Vehicle:
Centaure 1.
- CNES C81 Aeronomy mission - .
Nation: France.
Agency: CNES.
Apogee: 109 km (67 mi).
1969 July 10 - .
17:50 GMT - .
Launch Site:
Ile du Levant.
LV Family:
Belier.
Launch Vehicle:
Centaure 1.
- CNES C82 Aeronomy mission - .
Nation: France.
Agency: CNES.
Apogee: 114 km (70 mi).
1970 July 10 - .
- Indian General Lal tours space facilities. - .
Nation: Russia.
Related Persons: Nikolayev,
Sevastyanov,
Tereshkova.
The press conference behind them, Nikolayev and Tereshkova leave for Leningrad, and then on to Sochi for recuperation. General Lal from India tours Soviet space facilities. Smirnov proposes cooperation with India in space technology development..
1970 July 10 - .
00:30 GMT - .
Launch Site:
Woomera.
Launch Complex:
Woomera LA2.
Launch Pad: LA2 SL.
Launch Vehicle:
Skylark.
- X-ray spectra / Ionos X-ray astronomy / ionosphere mission - .
Nation: UK.
Agency: BAC.
Apogee: 203 km (126 mi).
1972 July 10 - .
11:00 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant III.
- Aeronomy / Solar Eclipse mission - .
Nation: Canada.
Agency: NRCC.
Apogee: 106 km (65 mi).
1972 July 10 - .
16:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 500 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-03-29 . USAF Sat Cat: 6097 . COSPAR: 1972-053A. Apogee: 548 km (340 mi). Perigee: 505 km (313 mi). Inclination: 74.00 deg. Period: 95.20 min. Possible navigation satellite. Replaced Cosmos 425..
1972 July 10 - .
18:51 GMT - .
Launch Site:
Poker Flat.
LV Family:
Sandhawk.
Launch Vehicle:
Terrier Sandhawk.
- Solar eclipse mission - .
Nation: USA.
Agency: Sandia.
Apogee: 300 km (180 mi).
1972 July 10 - .
19:50 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant III.
- Aeronomy / Solar Eclipse mission - .
Nation: Canada.
Agency: NRCC.
Apogee: 166 km (103 mi).
1972 July 10 - .
20:26 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant III.
- Aeronomy / Solar Eclipse mission - .
Nation: Canada.
Agency: NRCC.
Apogee: 103 km (64 mi).
1972 July 10 - .
20:29 GMT - .
Launch Site:
East Quoddy.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant III.
- Solar ultraviolet and x-ray mission - .
Nation: Canada.
Agency: NRCC.
Apogee: 143 km (88 mi).
1972 July 10 - .
21:32 GMT - .
Launch Site:
East Quoddy.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant III.
- Solar ultraviolet and x-ray mission - .
Nation: Canada.
Agency: NRCC.
Apogee: 148 km (91 mi).
1972 July 10 - .
21:39 GMT - .
Launch Site:
East Quoddy.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant III.
- Solar ultraviolet and x-ray mission - .
Nation: Canada.
Agency: NRCC.
Apogee: 144 km (89 mi).
1972 July 10 - .
21:41 GMT - .
Launch Site:
East Quoddy.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant III.
- Solar ultraviolet and x-ray mission - .
Nation: Canada.
Agency: NRCC.
Apogee: 152 km (94 mi).
1972 July 10 - .
22:01 GMT - .
Launch Site:
White Sands.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee 170.
- NRL NE4.246 Solar mission - .
Nation: USA.
Agency: NASA.
Apogee: 200 km (120 mi).
1972 July 10 - .
22:05 GMT - .
Launch Site:
White Sands.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee 170A.
- Solar mission - .
Nation: USA.
Agency: NASA.
Apogee: 200 km (120 mi).
1975 July 10 - .
08:00 GMT - .
Launch Site:
White Sands.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee 170.
- 13-in RC Flight 4 Astronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 179 km (111 mi).
1976 July 10 - .
- Death of Floyd L Thompson - .
Nation: USA.
Related Persons: Thompson, Floyd.
American engineer, at NASA 1927-1968, chief of flight research and then headed Langley..
1976 July 10 - .
01:14 GMT - .
Launch Site:
Kwajalein.
LV Family:
Deacon.
Launch Vehicle:
Rocketsonde.
- Arcasonde - .
Nation: USA.
Agency: MRN.
Apogee: 77 km (47 mi).
1977 July 10 - .
23:15 GMT - .
Launch Site:
Kwajalein.
LV Family:
Deacon.
Launch Vehicle:
Rocketsonde.
- Arcasonde - .
Nation: USA.
Agency: MRN.
Apogee: 79 km (49 mi).
1978 July 10 - .
LV Family:
Peacekeeper.
- Missile X flight computer contract. - .
SAMSO awarded a contract for the system definition phase of a Missile X flight computer to Autonetics Group of Rockwell International Corporation..
1979 July 10 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1113 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1979-07-23 . USAF Sat Cat: 11447 . COSPAR: 1979-064A. Apogee: 330 km (200 mi). Perigee: 173 km (107 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1979 July 10 - .
17:39 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF09.
Launch Pad: LF09?.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- OT GT40GM operational test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1979 July 10 - .
17:39 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF08.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- FOT GT68GM Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1980 July 10 - .
20:00 GMT - .
Launch Site:
Eareckson.
LV Family:
Deacon.
Launch Vehicle:
Rocketsonde.
- Arcasonde - .
Nation: USA.
Agency: MRN.
Apogee: 55 km (34 mi).
1981 July 10 - .
05:14 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Meteor 1-31 - .
Payload: Meteor-Priroda. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Class: Earth.
Type: Weather satellite. Spacecraft Bus: Meteor.
Spacecraft: Meteor-Priroda.
USAF Sat Cat: 12585 . COSPAR: 1981-065A. Apogee: 612 km (380 mi). Perigee: 574 km (356 mi). Inclination: 97.90 deg. Period: 96.50 min.
Also performed earth resources tasks. Acquisition of information required for continued investigation of the natural resources of the earth; development of remote sensing methods for measuring the parameters of the atmosphere and the earth's surface beneath the satellite. Carried scientific i nstruments developed in the People's Republic of Bulgaria, as well as Soviet equipment. Objects 1595 and 1596 launched by a single rocket.
- Iskra - .
Payload: RK-01. Mass: 28 kg (61 lb). Nation: Russia.
Agency: MOM.
Class: Materials.
Type: Materials science satellite. Spacecraft: Iskra.
Decay Date: 1990-04-16 . USAF Sat Cat: 19236 . COSPAR: 1981-065D. Apogee: 645 km (400 mi). Perigee: 618 km (384 mi). Inclination: 97.70 deg. Period: 97.34 min. Conduct of scientific experiments to study diffusion and heat processes in weightlessness..
1982 July 10 - .
09:57 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 14 - .
Payload: Progress s/n 117. Mass: 7,020 kg (15,470 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz T-5.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 33.65 days. Completed Operations Date: 1982-08-13 11:29:16 . Decay Date: 1982-08-13 11:29:16 . USAF Sat Cat: 13361 . COSPAR: 1982-070A. Apogee: 325 km (201 mi). Perigee: 301 km (187 mi). Inclination: 51.60 deg. Period: 90.70 min. Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 12 Jul 1982 11:41:00 GMT. Undocked on 10 Aug 1982 22:11:00 GMT. Destroyed in reentry on 13 Aug 1982 01:29:00 GMT. Total free-flight time 4.21 days. Total docked time 29.44 days..
1984 July 10 - .
Launch Site:
Tatishchevo.
LV Family:
UR-100N.
Launch Vehicle:
UR-100NU 15A35.
- ICBM operational test launch from missile base silo - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1985 July 10 - .
03:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1667 - .
Payload: Bion no. 7. Mass: 5,700 kg (12,500 lb). Nation: Russia.
Agency: MOM.
Class: Biology.
Type: Biology satellite. Spacecraft Bus: Vostok.
Spacecraft: Bion.
Duration: 6.90 days. Decay Date: 1985-07-17 . USAF Sat Cat: 15891 . COSPAR: 1985-059A. Apogee: 262 km (162 mi). Perigee: 206 km (128 mi). Inclination: 82.40 deg. Period: 89.20 min.
Biological research. Carried monkeys Verniy and Gordiy. Continued investigations of the influence of space flight factors on living organisms and radiation physics research. Cosmos 1667 was the second USSR biosatellite mission with a primate payload. Cosmos 1667 also featured a large rodent payload, however the U.S. only conducted a single experiment cardiovascular experiment on one of the two flight monkeys. Mission parameters were very similar to those of Cosmos 1514. Countries participating in the mission included the USSR, U.S., France, Czechoslovakia, the German Democratic Republic, Poland, Romania, Bulgaria and Hungary. Additional Details: here....
1986 July 10 - .
08:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1762 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Earth.
Type: Earth resources satellite. Spacecraft Bus: Vostok.
Spacecraft: Resurs F1-14F40.
Duration: 8.00 days. Decay Date: 1986-07-24 . USAF Sat Cat: 16855 . COSPAR: 1986-051A. Apogee: 263 km (163 mi). Perigee: 177 km (109 mi). Inclination: 82.50 deg. Period: 88.90 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation. .
1987 July 10 - .
12:12 GMT - .
Launch Site:
Andoya.
LV Family:
Viper.
Launch Vehicle:
Viper 3A.
- MAC-SINE S-F17 Aeronomy mission - .
Nation: USA.
Agency: DLR.
Apogee: 110 km (60 mi).
1987 July 10 - .
15:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1867 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: Plazma-A.
USAF Sat Cat: 18187 . COSPAR: 1987-060A. Apogee: 803 km (498 mi). Perigee: 776 km (482 mi). Inclination: 65.00 deg. Period: 100.70 min. Test of new Topaz reactor, new systems, and ion engines aboard US-AM bus - Tested Plasma-2 SPT electric engine..
1988 July 10 - .
Launch Site:
Thumba.
LV Family:
RH.
Launch Vehicle:
RH-200.
- Meteorological Chaff Meteorological mission - .
Nation: India.
Agency: ISRO.
Apogee: 70 km (43 mi).
1991 July 10 - .
14:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2153 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 247.00 days. Decay Date: 1992-03-13 . USAF Sat Cat: 21560 . COSPAR: 1991-049A. Apogee: 267 km (165 mi). Perigee: 182 km (113 mi). Inclination: 64.90 deg. Period: 89.00 min. Photo/digital surveillance..
1992 July 10 - .
- Giotto Flyby of Comet Grigg-Skjellerup - .
Nation: Europe.
Spacecraft: Giotto.
1995 July 10 - .
- Death of Vyecheslav Mikhailovich Kovtunenko - .
Nation: Russia.
Related Persons: Kovtunenko.
Russian chief designer. Chief Designer and General Designer of NPO Lavochkin 1977-1995. Kovtunenko started his career at the Yangel design bureau, where was responsible for satellite design..
1995 July 10 - .
12:38 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 401A/Centaur.
- USA 112 - .
Payload: Raven 2. Mass: 5,200 kg (11,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Naval signals intelligence satellite. Spacecraft: Raven satellite.
USAF Sat Cat: 23609 . COSPAR: 1995-034A. Apogee: 39,000 km (24,000 mi). Perigee: 1,000 km (600 mi). Inclination: 64.00 deg. Period: 720.00 min.
1997 July 10 - .
02:00 GMT - .
Launch Site:
Ryori.
LV Family:
MT-135.
Launch Vehicle:
MT-135P.
- Meteorological mission - .
Nation: Japan.
Agency: JMA.
Apogee: 53 km (32 mi).
1998 July 10 - .
- Death of Albert E Schuler - .
Nation: Germany,
USA.
Related Persons: Schuler.
German engineer in WW2, member of the Rocket Team in the United States thereafter..
1998 July 10 - .
06:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Resurs-O1 No. 4 - .
Payload: Resurs-O1 No. 4. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: RAKA.
Manufacturer: VNIIEM.
Program: Resurs.
Class: Earth.
Type: Earth resources satellite. Spacecraft Bus: Meteor.
Spacecraft: Resurs-O1.
USAF Sat Cat: 25394 . COSPAR: 1998-043A. Apogee: 818 km (508 mi). Perigee: 815 km (506 mi). Inclination: 98.80 deg. Period: 101.20 min.
In addition to its remote sensing equipment, the satellite carried the Belgian LLMS (Little LEO Messaging System) communications payload for the IRIS system. The launch was critical in restoring confidence in the Zenit vehicle prior to planned commercial launches of Globalstar satellites from Baikonur and the first Sea Launch flights using a three-stage Zenit from a California-based floating launch platform. Expected life 3 to 5 years.
- SAFIR-2 - .
Mass: 60 kg (132 lb). Nation: Germany.
Agency: DLR.
Manufacturer: Bremen.
Class: Communications.
Type: Civilian store-dump communications satellite. Spacecraft: Safir satellite.
USAF Sat Cat: 25399 . COSPAR: 1998-043F. Apogee: 819 km (508 mi). Perigee: 815 km (506 mi). Inclination: 98.80 deg. Period: 101.20 min. Relay satellite built by OHB System of Bremen..
- WESTPAC - .
Mass: 24 kg (52 lb). Nation: Australia.
Agency: WPLTN.
Manufacturer: EOS,
RKA.
Class: Earth.
Type: Geodetic satellite. Spacecraft: GFZ-1.
USAF Sat Cat: 25398 . COSPAR: 1998-043E. Apogee: 819 km (508 mi). Perigee: 815 km (506 mi). Inclination: 98.80 deg. Period: 101.20 min.
Formerly known as WPLTN-1, this geodesy satellite was a copy of Potsdam's GFZ-1 satellite, a sphere covered with laser retroreflectors, with a different `Fizeau' corner cube design. It serves as a target for the Western Pacific Laser Tracking Network (WPLTN) and is a joint project of Electro Optic Systems of Queanbeyan, New South Wales, Australia, and the Russian Space Agency. Diameter is 0.24m.
- Fasat-Bravo - .
Mass: 50 kg (110 lb). Nation: Chile.
Agency: FACh.
Manufacturer: Surrey.
Program: Fasat.
Class: Communications.
Type: Amateur radio communications satellite. Spacecraft: SSTL-70.
USAF Sat Cat: 25395 . COSPAR: 1998-043B. Apogee: 820 km (500 mi). Perigee: 815 km (506 mi). Inclination: 98.80 deg. Period: 101.30 min. Customer: Chilean Air Force (FACH). Chile's second satellite carrying store and forward and Earth observation payloads, replacing those lost on FASat-Alpha. Still operational as of 2000..
Additional Details: here....
- Gurwin Techsat 1B - .
Mass: 50 kg (110 lb). Nation: Israel.
Agency: RVSN.
Manufacturer: Technion.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: Gurwin.
USAF Sat Cat: 25397 . COSPAR: 1998-043D. Apogee: 819 km (508 mi). Perigee: 817 km (507 mi). Inclination: 98.80 deg. Period: 101.30 min. Built by Technion-Israel Institute of Technology. Replaced earlier Russian-launched Techsat which failed to orbit in 1995..
1999 July 10 - .
08:45 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
Launch Pad: SLC17B.
LV Family:
Thor.
Launch Vehicle:
Delta 7420-10C.
- Globalstar 32 - .
Mass: 222 kg (489 lb). Nation: USA.
Agency: Globalstar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: Globalstar.
USAF Sat Cat: 25851 . COSPAR: 1999-037A. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.10 min.
- Globalstar 35 - .
Mass: 222 kg (489 lb). Nation: USA.
Agency: Globalstar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: Globalstar.
USAF Sat Cat: 25853 . COSPAR: 1999-037C. Apogee: 1,415 km (879 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.10 min.
- Globalstar 51 - .
Mass: 222 kg (489 lb). Nation: USA.
Agency: Globalstar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: Globalstar.
USAF Sat Cat: 25854 . COSPAR: 1999-037D. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.10 min.
- Globalstar 30 - .
Mass: 222 kg (489 lb). Nation: USA.
Agency: Globalstar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: Globalstar.
USAF Sat Cat: 25852 . COSPAR: 1999-037B. Apogee: 1,415 km (879 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.10 min.
2002 July 10 - .
- Shuttle fleet grounded. - .
Nation: USA.
Program: ISS.
Flight: STS-111 ISS EO-5.
The Shuttle fleet was grounded for several weeks when cracks were found in the flowliners of the liquid hydrogen lines within the shuttles. These lines supplied cold liquid hydrogen from the external tank to the shuttle engines. After several weeks of study NASA concluded that they could be fixed by welding, but the problem delayed the next ISS assembly mission and pushed the STS-107 Columbia science mission into 2003.
2005 July 10 - .
03:30 GMT - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima M-V.
Launch Vehicle:
M-V.
- Suzaku - .
Payload: Astro E2. Mass: 1,680 kg (3,700 lb). Nation: Japan.
Agency: JAXA.
Manufacturer: Toshiba.
Class: Astronomy.
Type: X-ray astronomy satellite. Spacecraft Bus: Astro.
Spacecraft: ASTRO E.
USAF Sat Cat: 28773 . COSPAR: 2005-025A. Apogee: 573 km (356 mi). Perigee: 562 km (349 mi). Inclination: 31.40 deg. Period: 96.00 min.
Delayed from February, June 26, July 6 and 8, 2005. CUTE-1.7 nanosat mistakenly reported on this flight. Astro-E2 was renamed Suzaku (after a legendary red bird) after launch. It replaced the Astro-E, which never reached orbit due to an M-V-4 launch failure in 2000. The satellite had five 0.4-meter diameter X-ray telescopes, one with an XRS microcalorimeter and the other four with X-ray CCD cameras. However it was revealed that the XRS failed on 9 August due to leaking of helium coolant.
2006 July 10 - .
- STS-121 - Wakeup Song: Clocks - .
Flight: STS-121.
"Clocks" by Coldplay for Mission Specialist Piers Sellers. Requested by his family..
2006 July 10 - .
07:14 GMT - .
- EVA STS-121-2 - .
Crew: Fossum,
Sellers.
EVA Duration: 0.28 days. Nation: USA.
Related Persons: Fossum,
Sellers.
Program: ISS.
Flight: STS-121.
The crew worked on the exterior of the ISS. They installed a spare pump module on the ESP-2 platform and replaced an umbilical cable assembly for the ISS Mobile Transporter, making it ready for installation of new solar truss panels on the next mission..
2006 July 10 - .
12:08 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota SLP.
Launch Vehicle:
GSLV.
FAILURE: One of the liquid-fueled strap-on motors failed to develop thrust. By 40 seconds after launch the GSLV had veered outside of the launch corridor and the destruct signal was sent..
Failed Stage: 0.
- Insat 4C - .
Mass: 2,168 kg (4,779 lb). Nation: India.
Agency: ISRO.
Program: Insat.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: I-2K.
2008 July 10 - .
- EVA ISS EO-17-1 - .
Crew: Kononenko,
Volkov, Sergey.
EVA Duration: 0.26 days. Nation: Russia.
Related Persons: Kononenko,
Volkov, Sergey.
Program: ISS.
Flight: Soyuz TMA-12.
Inspected the Soyuz TMA-12 spacecraft in an attempt to determine the reason for the failure of the service module to separate on earlier missions, removed a pyrotechnic bolt from the struts connecting the service and reentry modules of the Soyuz for examination on earth, and installed a docking target for the future Russian Multipurpose Research Module.
2010 July 10 - .
07:32 GMT - .
Launch Site:
Bay of Biscay Launch Area.
Launch Platform: S612.
Launch Vehicle:
MSBS M51.
- RV x 6 - .
Nation: France.
Agency: DMA.
Apogee: 1,000 km (600 mi). Operational test..
2010 July 10 - .
18:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/39.
Launch Pad: LC200/39.
LV Family:
Proton.
Launch Vehicle:
Proton-M/Briz-M.
- Echostar 15 - .
Mass: 5,520 kg (12,160 lb). Nation: USA.
Agency: ILS.
Program: Echostar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: FS-1300.
USAF Sat Cat: 36792 . COSPAR: 2010-034A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.10 deg. Period: 1,436.00 min. Supported Dish direct-to-home broadcast network to North America..
2011 July 10 - .
14:00 GMT - .
Launch Site:
Wallops Island.
Launch Complex:
Wallops Island LA2.
LV Family:
Hawk.
Launch Vehicle:
Terrier Improved Orion.
- NASA 41.090GE - .
Nation: USA.
Apogee: 158 km (98 mi). Ionosphere mission..
2011 July 10 - .
14:00 GMT - .
Launch Site:
Wallops Island.
Launch Complex:
Wallops Island LA2.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant VC.
- NASA 21.140GE - .
Nation: USA.
Apogee: 158 km (98 mi). Ionosphere mission..
2014 July 10 - .
18:55 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELS.
LV Family:
R-7.
Launch Vehicle:
Soyuz-ST-B.
- O3b FM3 - .
Mass: 700 kg (1,540 lb). Nation: UK.
Spacecraft: ELiTeBus.
USAF Sat Cat: 40079 . COSPAR: 2014-038A. Apogee: 8,069 km (5,013 mi). Perigee: 8,062 km (5,009 mi). Inclination: 0.0300 deg. Period: 287.93 min.
- O3b FM7 - .
Mass: 700 kg (1,540 lb). Nation: UK.
Spacecraft: ELiTeBus.
USAF Sat Cat: 40080 . COSPAR: 2014-038B. Apogee: 8,071 km (5,015 mi). Perigee: 8,061 km (5,008 mi). Inclination: 0.0300 deg. Period: 287.93 min.
- O3b FM6 - .
Mass: 700 kg (1,540 lb). Nation: UK.
Spacecraft: ELiTeBus.
USAF Sat Cat: 40081 . COSPAR: 2014-038C. Apogee: 8,069 km (5,013 mi). Perigee: 8,063 km (5,010 mi). Inclination: 0.0300 deg. Period: 287.93 min.
- O3b FM8 - .
Mass: 700 kg (1,540 lb). Nation: UK.
Spacecraft: ELiTeBus.
USAF Sat Cat: 40082 . COSPAR: 2014-038D. Apogee: 8,071 km (5,015 mi). Perigee: 8,061 km (5,008 mi). Inclination: 0.0300 deg. Period: 287.93 min.
2015 July 10 - .
16:28 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota SLP.
Launch Pad: Sriharikota FLP.
LV Family:
PSLV.
Launch Vehicle:
PSLV-XL.
- DMC3-1 - .
Payload: SSTL-300-S1. Mass: 440 kg (970 lb). Nation: UK.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SSTL-300.
USAF Sat Cat: 40715 . COSPAR: 2015-032A. Apogee: 660 km (410 mi). Perigee: 638 km (396 mi). Inclination: 98.04 deg. Period: 97.71 min.
Third generation Disaster Monitoring Constellation. The three satellites were deployed on a single launch. DMC Imaging International was a
Surrey Satellite spinoff which operated the DMC imaging
satellites in collaboration with several developing countries. The
satellites have the capability to return prompt imaging of areas in
those countries affected by natural disasters. The SSTL-300S1 platform provided 45 degree fast slew off-pointing and was capable of acquiring multiple targets in one pass using multiple viewing modes. The high resolution imager on board the satellites was designed and manufactured by SSTL and provided 1 meter resolution in panchromatic mode, and 4 meter resolution in multispectral mode, with a swath width of 23.4km.
The three satellites were phased 120 degrees apart around the same sun synchronous orbit with a 22:10 local time longitude of descending node sun synchronous orbit. This was acommplished using their on board propulsion systems in the three months after the launch. With off-pointing capability, the DMC3/TripleSat Satellite Constellation was able to target anywhere on Earth once per day.
- DMC3-2 - .
Payload: SSTL-300-S1. Mass: 440 kg (970 lb). Nation: UK.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SSTL-300.
USAF Sat Cat: 40716 . COSPAR: 2015-032B. Apogee: 659 km (409 mi). Perigee: 640 km (390 mi). Inclination: 98.03 deg. Period: 97.71 min. 22:10 local time longitude of descending node sun synchronous orbit..
- DMC3-3 - .
Payload: SSTL-300-S1. Mass: 440 kg (970 lb). Nation: UK.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SSTL-300.
USAF Sat Cat: 40717 . COSPAR: 2015-032C. Apogee: 662 km (411 mi). Perigee: 637 km (395 mi). Inclination: 98.10 deg. Period: 97.71 min. 22:10 local time longitude of descending node sun synchronous orbit..
- CBNT-1 - .
Mass: 91 kg (200 lb). Nation: UK.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: CBNT.
USAF Sat Cat: 40718 . COSPAR: 2015-032D. Apogee: 659 km (409 mi). Perigee: 636 km (395 mi). Inclination: 98.03 deg. Period: 97.67 min. Surrey Satellite Technology experimental imaging satellite. SSTL did not disclose the meaning of the CBNT abbreviation. 22:10 local time longitude of descending node sun synchronous orbit..
- DeOrbitSail - .
Mass: 3.00 kg (6.60 lb). Nation: UK.
Class: Technology.
Type: Technology satellite. Spacecraft: CubeSat.
USAF Sat Cat: 40719 . COSPAR: 2015-032E. Apogee: 657 km (408 mi). Perigee: 634 km (393 mi). Inclination: 98.04 deg. Period: 97.63 min. 3U cubesat. 22:10 local time longitude of descending node sun synchronous orbit..
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