Encyclopedia Astronautica
August 11


August 11 Chronology


1933 August 11 - . Launch Vehicle: GIRD-09. FAILURE: Failure.
  • GIRD-09 launch attempt. - . Nation: USSR. Summary: Launch failure..

1933 August 11 - . Launch Vehicle: Magdeburg.
  • Nebel rocket - . Nation: Germany. Apogee: 0.0020 km (0.0012 mi). Summary: Second attempt from Schwielow Lake. The rocket goes horizontal and hits the water in the lake's steamboat channel. It cannot be recovered..

1950 August 11 - .
  • XS-1 Flight 140 - . Crew: Griffith. Payload: XS-1 # 2 flight 59. Nation: USA. Related Persons: Griffith. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: NACA flight 39. For pressure distribution and stability and control data. Check of stabilizer effectiveness. .

1952 August 11 - . Launch Site: White Sands. LV Family: Honest John. Launch Vehicle: Honest John. LV Configuration: Honest John 47.
  • Test mission - . Nation: USA. Apogee: 10 km (6 mi).

1953 August 11 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1208E.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1954 August 11 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 2527R.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1957 August 11 - . 05:16 GMT - . Launch Site: Atlantic Ocean. Launch Pad: 70.4 N x 57.0 W. Launch Platform: LSD-29. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon II5.10F. FAILURE: Failure.
  • SUI 65 Aeronomy / Chemical release mission - . Nation: USA. Agency: SUI. Apogee: 0 km ( mi). Summary: Launched at IGY Rockoon Launch Site 1, Atlantic Ocean LP10 - - Latitude: 70.40 N - Longitude: 57.00 W..

1957 August 11 - . 20:30 GMT - . Launch Site: Atlantic Ocean. Launch Pad: 66.7 N x 54.9 W. Launch Platform: LSD-29. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon II5.11F.
  • SUI 66 Aeronomy / Chemical release mission - . Nation: USA. Agency: SUI. Apogee: 100 km (60 mi). Summary: Launched at IGY Rockoon Launch Site 1, Atlantic Ocean LP11 - - Latitude: 66.67 N - Longitude: 54.93 W..

1958 August 11 - . 09:30 GMT - . Launch Site: Johnston Island. LV Family: Doorknob. Launch Vehicle: Doorknob 2. LV Configuration: Doorknob-2.
  • Aeronomy mission - . Nation: USA. Agency: Sandia. Apogee: 83 km (51 mi).

1959 August 11 - . 18:01 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC13. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 14D.
  • Research and development launch - . Nation: USA. Agency: USAF. Apogee: 1,800 km (1,100 mi).

1960 August 11 - . LV Family: Atlas. Launch Vehicle: Atlas D.
  • Mercury-Atlas 1 (MA-1) mission malfunction discussed. - . Nation: USA. Related Persons: Chamberlin. Program: Mercury. Summary: Representatives of NASA, McDonnell, Ballistic Missile Division, Space Technology Laboratories, and Convair met at Cape Canaveral and later at Convair Astronautics (Aug. 30, 1960) to discuss the Mercury-Atlas 1 (MA-1) mission malfunction. . Additional Details: Mercury-Atlas 1 (MA-1) mission malfunction discussed..

1961 August 11 - .
1961 August 11 - . 14:30 GMT - . Launch Site: Eglin. Launch Vehicle: Exos. LV Configuration: Exos CRL AA13.194.
  • Ion density Test / ionosphere mission - . Nation: USA. Agency: USAF. Apogee: 114 km (70 mi).

1962 August 11 - .
  • NASA schedule for Apollo command and service modules - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. A NASA program schedule for the Apollo spacecraft command and service modules through calendar year 1965 was established for financial planning purposes and distributed to the NASA Office of Manned Space Flight, Marshall Space Flight Center, and MSC. The key dates were: complete service module drawing release, May 1, 1963; complete command module drawing release, June 15, 1963; manufacture complete on the first spacecraft, February 1, 1964; first manned orbital flight, May 15, 1965. This tentative schedule depended on budget appropriations.

1962 August 11 - .
  • Eight companies to bid on Apollo lunar excursion module - . Nation: USA. Program: Apollo. Spacecraft: Apollo LM; LM Source Selection. Of the 11 companies invited to bid on the lunar excursion module on July 25, eight planned to respond. NAA had notified MSC that it would not bid on the contract. No information had been received from the McDonnell Aircraft Corporation and it was questionable whether the Northrop Corporation would respond.

1962 August 11 - . 01:48 GMT - . Launch Site: Kronogard. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun K-62-3.
  • Air sample Aeronomy mission - . Nation: Sweden. Agency: RTG; AFCRL. Apogee: 105 km (65 mi).

1962 August 11 - . 08:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Vostok 8K72K.
  • Vostok 3 - . Call Sign: Sokol (Falcon ). Crew: Nikolayev. Backup Crew: Bykovsky; Volynov. Payload: Vostok 3KA s/n 5. Mass: 4,722 kg (10,410 lb). Nation: USSR. Related Persons: Nikolayev; Bykovsky; Popovich; Gagarin; Smirnov; Barmin; Kirillov; Khrushchev; Kozlov, Frol; Ustinov; Volynov. Agency: RVSN. Program: Vostok. Class: Manned. Type: Manned spacecraft. Flight: Vostok 3. Spacecraft: Vostok. Duration: 3.93 days. Decay Date: 1962-08-15 . USAF Sat Cat: 363 . COSPAR: 1962-A-Mu-1. Apogee: 218 km (135 mi). Perigee: 166 km (103 mi). Inclination: 65.0000 deg. Period: 88.30 min. Joint flight with Vostok 4. The first such flight, where Vostok capsules were launched one day apart, coming within a few kilometers of each other at the orbital insertion of the second spacecraft. The flight was supposed to occur in March, but following various delays, one of the two Vostok pads was damaged in the explosion of the booster of the third Zenit-2 reconnsat in May. Repairs were not completed until August. Vostok 3 studied man's ability to function under conditions of weightlessness; conducted scientific observations; furthered improvement of space ship systems, communications, guidance and landing. Immediately at orbital insertion of Vostok 4, the spacecraft were less than 5 km apart. Popovich made radio contact with Cosmonaut Nikolayev. Nikolayev reported shortly thereafter that he had sighted Vostok 4. Since the Vostok had no maneuvering capability, they could not rendezvous or dock, and quickly drifted apart. The launches did allow Korolev to offer something new and different, and gave the launch and ground control crews practice in launching and handling more than one manned spacecraft at a time. The cosmonaut took colour motion pictures of the earth and the cabin interior. Additional Details: Vostok 3.

1963 August 11 - .
  • Kamanin picks up a new Volga automobile. - . Nation: USSR. Related Persons: Tereshkova; Bykovsky; Korolev. Flight: Vostok 6; Vostok 7; Vostok 8; Vostok 9; Vostok 10. Kamanin picks up a new Volga automobile. It cost him 5513 roubles, but one door doesn't fit and the trunk is scarred with excess hardened resin. Sukarno has asked for Tereshkova and Bykovskiy to visit Indonesia for two weeks in August, but this is impossible.

    In a three hour meeting Korolev goes over his future flight plans for Vostok. The first flight will be unmanned, with a biological payload, in February or March 1964. The flight is to last 10 or 11 days and take the specimens up to 600 to 1000 km altitude, into the lower reaches of the Van Allen radiation belts. This will be followed by three cosmonaut flights of ten days with significant military and scientific experiments. A new ground control system will be installed and tested to handle all in-flight emergencies. A new autonomous on-board navigation system will be flight tested. Korolev wants the military to take over conduct of future Vostok flights - they are taking up to much of his time and nerves. He has told this repeated to Khrushchev and Brezhnev without result. Meanwhile Kamanin lobbies within the military hierarchy for the removal of Odintsev. It is decided that the matter will be taken up at the next meeting of the Military Soviet.


1964 August 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-C. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II B-9.
  • Double Talley - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). Summary: Demonstration and shakedown operations launch.

1964 August 11 - . 02:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/22. LV Family: Tsiklon. Launch Vehicle: R-36 8K67. FAILURE: Failure.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1964 August 11 - . 05:10 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 7C. LV Configuration: Skylark-7C SL301.
  • LUX Solar AC1 Solar x-ray and ultraviolet mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 145 km (90 mi).

1964 August 11 - . 10:30 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.82GG.
  • Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 172 km (106 mi).

1965 August 11 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC29A. LV Family: Polaris. Launch Vehicle: Polaris A1. LV Configuration: Polaris A1 C2X-3.
  • STAFF 3 test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1965 August 11 - . 01:35 GMT - . Launch Site: Pameungpeuk. LV Family: Kappa. Launch Vehicle: Kappa 8. LV Configuration: Kappa 8 K-8(L)-4.
  • SK-8-4 Aeronomy / ionosphere / Fields mission - . Nation: Japan. Agency: ISAS. Apogee: 191 km (118 mi).

1965 August 11 - . 11:49 GMT - . Launch Site: White Sands. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.144GM.
  • Meteoroids Aeronomy / meteorites mission - . Nation: USA. Agency: NASA. Apogee: 129 km (80 mi).

1965 August 11 - . 14:31 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas Centaur D. LV Configuration: Atlas Centaur D AC-6 / Centaur D 151D.
  • Surveyor; Atlas Centaur 6 - . Payload: Surveyor-SD-2. Mass: 950 kg (2,090 lb). Nation: USA. Agency: NASA; JPL. Class: Moon. Type: Lunar probe. Spacecraft: Surveyor. USAF Sat Cat: 1503 . COSPAR: 1965-064A. Summary: Centaur AC-6 launched dummy Surveyor payload into a barycentric / translunar orbit..

1966 August 11 - . Launch Site: Barking Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-86.
  • ACS technology mission - . Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi).

1966 August 11 - . 12:05 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 8L. LV Configuration: Kappa 8L K-8L-10.
  • Aeronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 130 km (80 mi).

1966 August 11 - . 15:53 GMT - . Launch Site: Fort Churchill. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 CRL AC3.364.
  • Auroral emissions Aurora mission - . Nation: USA. Agency: AFCRL. Apogee: 207 km (128 mi).

1966 August 11 - . 17:44 GMT - . Launch Site: Delamar Dry Lake DZ. Launch Pad: 37.3 N x 114.9 W. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 1-66-111.
  • X-15A HS,MuMet,SB,Gas Technology/Meteor/Aeronomy mission - . Nation: USA. Agency: NASA; USAF. Apogee: 76 km (47 mi). Summary: Maximum Speed - 5776 kph. Maximum Altitude - 76500 m. Record dynamic pressure..

1967 August 11 - . 09:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.223NA.
  • LUSTER II 1967 Meteorites mission - . Nation: USA. Agency: NASA. Apogee: 141 km (87 mi).

1967 August 11 - . 20:25 GMT - . Launch Site: Indian Ocean. Launch Pad: 20.0 S x 65.0 E. Launch Platform: VOKV. LV Family: M-100. Launch Vehicle: M-100.
  • Ionosphere mission - . Nation: USSR. Agency: AN. Apogee: 90 km (55 mi).

1968 August 11 - . 07:04 GMT - . Launch Site: Natal. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL AG07.274.
  • Meteorites Meteorites mission - . Nation: USA. Agency: USAF. Apogee: 98 km (60 mi).

1969 August 11 - . 01:30 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna C. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C51/1.
  • ESRO C51 / 1 Aeronomy mission - . Nation: Europe. Agency: ESRO. Apogee: 112 km (69 mi).

1969 August 11 - . 15:30 GMT - . Launch Site: ETR Launch Area. Launch Platform: UK S26. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3E.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1970 August 11 - .
  • X-24 Flight 16 - . Crew: Manke. Payload: X-24A flight 16. Nation: USA. Related Persons: Manke. Class: Manned. Type: Manned spaceplane. Spacecraft: X-24A. Summary: Maximum Speed - 1047 kph. Maximum Altitude - 19477 m. Flight Time - 413 sec..

1970 August 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • OT GT06F operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1971 August 11 - . 09:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 89 km (55 mi).

1972 August 11 - .
  • Soyuz 7K-S designs completed - . Nation: USSR. Spacecraft: Soyuz 7K-S; Soyuz OB-VI. The Soyuz 7K-S had two parallel designs - the base variant, which was for special-purpose military solo missions; and a space station transport variant 7K-ST. The Soyuz 7K-S program was to consist of four unmanned, followed by two manned test flights, then two operational launches.

1972 August 11 - .
  • M2 Flight 31 - . Crew: Dana. Payload: M2-F3 flight 15. Nation: USA. Related Persons: Dana. Program: NASA Lifting Body. Class: Manned. Type: Manned spaceplane. Spacecraft: M2-F3. Summary: Maximum Speed - 1168 kph. Maximum Altitude - 20480 m. Flight Time - 375 sec..

1972 August 11 - . 01:01 GMT - . Launch Site: Syowa Base. LV Family: S. Launch Vehicle: S-210. LV Configuration: S-210JA-8.
  • Ionosphere / fields mission - . Nation: Japan. Agency: NIPR. Apogee: 127 km (78 mi).

1973 August 11 - . 05:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHIR. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 86 km (53 mi).

1975 August 11 - . 16:51 GMT - . Launch Site: Wallops Island. LV Family: Loki. Launch Vehicle: Super Loki. LV Configuration: Super Loki T 1-8409.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 54 km (33 mi).

1976 August 11 - . 19:12 GMT - . Launch Site: Wallops Island. LV Family: Terrier. Launch Vehicle: Terrier Malemute. LV Configuration: Terrier Malemute NASA 12.36GT.
  • Test mission - . Nation: USA. Agency: NASA. Apogee: 612 km (380 mi).

1977 August 11 - . 21:22 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 70 km (43 mi).

1978 August 11 - .
  • Complete test preparation, STA-099 - . Nation: USA. Program: STS.

1978 August 11 - .
  • Complete forward RCS, Columbia (OV-102) - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Columbia.

1978 August 11 - .
  • Complete forward RCS thermal test - . Nation: USA. Program: STS.

1978 August 11 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Combat training launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978 August 11 - . 02:20 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC25C. LV Family: Trident. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 C4X-18.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1979 August 11 - .
  • Ferry flight, Atlanta to St. Louis - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise. Summary: Ferry flight, shuttle carrier aircraft/Enterprise (OV-101), Atlanta to St. Louis (1 hour, 50 minutes).

1979 August 11 - . 09:15 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1120 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4MKM. Duration: 13.00 days. Decay Date: 1979-08-24 . USAF Sat Cat: 11485 . COSPAR: 1979-073A. Apogee: 362 km (224 mi). Perigee: 170 km (100 mi). Inclination: 70.6000 deg. Period: 89.80 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1980 August 11 - . 13:44 GMT - . Launch Site: Antigua. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 72 km (44 mi).

1981 August 11 - . 20:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 89 km (55 mi).

1982 August 11 - . 00:35 GMT - . Launch Site: Poker Flat. LV Family: Honest John. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.29UL.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1982 August 11 - . 23:30 GMT - . Launch Site: Kiruna. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P214K.
  • CAMP Aeronomy mission - . Nation: UK. Agency: SRC. Apogee: 129 km (80 mi).

1987 August 11 - . 19:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 90 km (55 mi).

1988 August 11 - . 17:37 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 63 km (39 mi).

1989 August 11 - . 14:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 62 km (38 mi).

1990 August 11 - . 08:10 GMT - . Launch Site: Kwajalein. Launch Complex: Kwajalein RN. LV Family: Tomahawk Sandia. Launch Vehicle: Taurus Tomahawk Nike. LV Configuration: Taurus Nike Tomahawk NASA 38.17UE.
  • CRRES AA-5 Plasma mission - . Nation: USA. Agency: NASA. Apogee: 375 km (233 mi).

1991 August 11 - . 12:37 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 75 km (46 mi).

1991 August 11 - .
1993 August 11 - .
  • Mir News 184: Progress-M19 - . Nation: Russia. Program: Mir. Flight: Mir EO-14. This freighter has been launched from Baykonur on 10.08.93 at 2223 UTC (for Moscow and TsUP-time already 11.08.93) for a 2-days flight to the Mir-station. Perhaps there has been a slight delay for I expected the launch at 2216 UTC. Somewhat later than expected I monitored the transmissions of Progress-M19 on 922.755 mc and in the 166 and 165 mc bands between 0256 and 0301 UTC. To enable Progress-M19 to dock to the forward docking port of Mir (transition section P.Kh.O.) the old Progress-M still docked to that port has to disappear soon. This undocking is scheduled for 11.08.93 at 1534 UTC.

    Perseid-meteorites: These meteorites coming from the comet Swift- Tuttle are visible (clouds permitting) around 12 august every year. Thus far clouds did not permit this for us this year, but the Mir-cosmonauts, not hindered by clouds or fog, were able to see the meteorites. Tsibliyev, the captain of the Mir-station, reported during the pass in orbit 42770, 11.08.93, 0452-0503 UTC, that they saw a little bit of it. He added that he had to report some 'battle wounds'. He told TsUP that the station had been hit by 4 particles obviously coming from that meteorite-rain. They caused minor damages to 2 solar batteries (on the base block and on Kristall - Module-T) and to one of the portholes. The window of that porthole showed a cavern with a diameter of 2 a 3 mm. T. nor TsUP did not show any concern. To be realistic: thus far we have to do with minor particles, but bigger particles can cause serious damages to space-ships and stations, even leakage and consequently decompression. In my opinion the recent experience of the Mir-crew fully justifies NASA's decision to put back the launch of Space shuttle Discovery until 12.08.93 due to concern for that meteorite-storm.

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


1994 August 11 - . 15:27 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 367-02.
  • Cosmos 2287 - . Payload: Glonass s/n 67L. Mass: 1,400 kg (3,000 lb). Nation: Russia. Agency: MOM. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass . USAF Sat Cat: 23203 . COSPAR: 1994-050A. Apogee: 19,142 km (11,894 mi). Perigee: 19,118 km (11,879 mi). Inclination: 64.9000 deg. Period: 675.70 min. Summary: Glonass navigation satellite. .
  • Cosmos 2288 - . Payload: Glonass s/n 70L. Mass: 1,400 kg (3,000 lb). Nation: Russia. Agency: MOM. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 23204 . COSPAR: 1994-050B. Apogee: 19,168 km (11,910 mi). Perigee: 19,091 km (11,862 mi). Inclination: 64.8100 deg. Period: 675.73 min. Summary: Glonass navigation satellite..
  • Cosmos 2289 - . Payload: Glonass s/n 75L. Mass: 1,400 kg (3,000 lb). Nation: Russia. Agency: MOM. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 23205 . COSPAR: 1994-050C. Apogee: 19,133 km (11,888 mi). Perigee: 19,126 km (11,884 mi). Inclination: 64.8100 deg. Period: 675.73 min. Summary: Glonass navigation satellite..

1997 August 11 - . 13:38 GMT - . Launch Site: Wallops Island. LV Family: Loki. Launch Vehicle: Super Loki. LV Configuration: Super Loki Falling Sphere.
  • CRISTA Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 107 km (66 mi).

1997 August 11 - . 13:43 GMT - . Launch Site: Wallops Island. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A Falling Sphere.
  • CRISTA Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 119 km (73 mi).

1997 August 11 - . 18:18 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.164US.
  • USC-2 SOHO Cal Solar extreme ultraviolet mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 307 km (190 mi).

1997 August 11 - . 21:34 GMT - . Launch Site: Wallops Island. LV Family: Loki. Launch Vehicle: Super Loki. LV Configuration: Super Loki Falling Sphere.
  • CRISTA Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 106 km (65 mi).

1999 August 11 - .
  • Death of Robert 'RT' Jones - . Nation: USA. Related Persons: Jones, Robert. Summary: American engineer, credited by NASA as inventor of the swept-back and oblique wing concepts..

2001 August 11 - .
2003 August 11 - .
  • Galileo Enters Solar Conjunction - . Nation: USA. Spacecraft: Galileo.

2004 August 11 - . Launch Site: Sriharikota. LV Family: Shahab. Launch Vehicle: Shahab 3.
  • - . Nation: Iran. Apogee: 150 km (90 mi). Summary: Missile demonstration flight. Stretched Shahab-3 launched into Dasht-E-Kavir desert..

2004 August 11 - . 05:01 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz-U D15000-685.
  • Progress M-50 - . Payload: Progress M s/n 250. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RAKA. Manufacturer: Korolev. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-9. Spacecraft: Progress M. Duration: 133.73 days. Decay Date: 2004-12-23 . USAF Sat Cat: 28399 . COSPAR: 2004-032A. Apogee: 365 km (226 mi). Perigee: 358 km (222 mi). Inclination: 51.6000 deg. Period: 91.80 min. Summary: Delayed from July 22 and 28. Docked with the International Space Station at 05:01 GMT on August 14. Undocked from the Zvezda module of the ISS on December 22 at 19:34 GMT and was deorbited over the Pacific at 22:32 GMT..

2004 August 11 - . 10:25 GMT - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU.
  • Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

2005 August 11 - . 08:20 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5GS. LV Configuration: Ariane 5GS V166 (523).
  • Ipstar 1 - . Payload: Thaicom 4, LS-1300SX. Mass: 6,486 kg (14,299 lb). Nation: Thailand. Agency: Shinawat. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28786 . COSPAR: 2005-028A. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Ariane 5GS version maiden flight. Launch delayed from July 8 and 11, 2005. Heaviest geosynchronous transfer orbit payload to date. As of 2007 Mar 11 located at 119.46E drifting at 0.009W degrees per day..

2006 August 11 - . 22:15 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA V172 (531).
  • JCSAT 10 - . Payload: AS2100AX. Mass: 4,048 kg (8,924 lb). Nation: Japan. Agency: JSAT. Manufacturer: Lockheed. Program: JCSAT. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 29272 . COSPAR: 2006-033A. Apogee: 35,793 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Ku/C-band television broadcasting satellite for the Japanese market; mass 1858 kg dry. As of 2007 Mar 11 located at 128.01E drifting at 0.012W degrees per day..
  • Syracuse 3B - . Payload: Spacebus 4000B3. Mass: 3,750 kg (8,260 lb). Nation: France. Agency: DGA. Manufacturer: Alenia. Program: Syracuse. Class: Communications. Type: Military communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 29273 . COSPAR: 2006-033B. Apogee: 35,796 km (22,242 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: SHF and EHF military communications links for the French military. As of 2007 Mar 9 located at 5.21W drifting at 0.004W degrees per day..

2007 August 11 - . 16:28 GMT - .
2009 August 11 - . 04:50 GMT - . Launch Site: San Nicolas. LV Family: Black Brant. Launch Vehicle: Black Brant 9.
  • NASA 36.229DR - . Mass: 150 kg (330 lb). Nation: USA. Agency: MDA. Summary: ABM target.

2009 August 11 - . 19:47 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton/Briz M s/n P347.
  • Asiasat 5 - . Mass: 3,760 kg (8,280 lb). Nation: Russia. Agency: ILS. Program: Asiasat. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 35696 . COSPAR: 2009-042A. Apogee: 35,791 km (22,239 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Provided C-band and Ku-band communications services..

2010 August 11 - .
  • EVA ISS EO-24-3 - . Crew: Wheelock; Caldwell. EVA Type: Extravehicular activity. EVA Duration: 0.31 days. Nation: USA. Program: ISS. Flight: ISS EO-24; ISS EO-23. Summary: Removed failed ammonia pump on the S1 truss and began installation of replacement..

2011 August 11 - . 14:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC8. LV Family: Minotaur. Launch Vehicle: Minotaur 4. LV Configuration: Minotaur 4 Lite.
  • HTV-2b - . Nation: USA. Apogee: 100 km (60 mi). Summary: Test mission. Hypersonic glider was launched from Vandenberg across the Pacific. The mission ended prematurely with loss of signal three minutes into the glider's free flight..

2011 August 11 - . 16:15 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3B.
  • Paksat 1R - . Mass: 5,120 kg (11,280 lb). Nation: Pakistan. Class: Communications. Type: Communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 37779 . COSPAR: 2011-042A. Apogee: 35,793 km (22,240 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.00 min. Summary: Communications satellite to replace Paksat 1, the former Palapa C1..

Home - Browse - Contact
© / Conditions for Use