Encyclopedia Astronautica
August 06


August 06 Chronology


1913 August 6 - .
1914 August 6 - .
1945 August 6 - .
  • U.S. drops atomic bomb on Japanese city of Hiroshima - . Nation: Japan.

1947 August 6 - .
  • XS-1 Flight 38 - . Crew: Yeager. Payload: XS-1 # 1 flight 20. Nation: USA. Related Persons: Yeager. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: AF glide flight 1. Pilot familiarization..

1948 August 6 - . 01:37 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-N-8. LV Configuration: Aerobee RTV-N-8 NRL 1.
  • Aerobee Venus 1 Aeronomy / solar ultraviolet mission - . Nation: USA. Agency: NRL. Apogee: 98 km (60 mi). Summary: Solar radiation, pressure, temperature research. Launched at 1837 local time. Reached 96.6 km..

1950 August 6 - .
  • Birth of Winston Elliott Scott - . Nation: USA. Summary: African-American test pilot mission specialist astronaut. Flew on STS-72, STS-87..

1952 August 6 - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Double Deacon.
  • B-58 Model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1953 August 6 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Snark. Launch Vehicle: Snark. LV Configuration: Snark N-69A GM-3391.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 10 km (6 mi).

1954 August 6 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 2756T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1957 August 6 - . 10:52 GMT - . Launch Site: Atlantic Ocean. Launch Pad: 62.3 N x 56.3 W. Launch Platform: LSD-29. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon II5.03F.
  • SUI 58 Aeronomy / aurora / chemical release mission - . Nation: USA. Agency: SUI. Apogee: 116 km (72 mi). Summary: Launched at IGY Rockoon Launch Site 1, Atlantic Ocean LP3 - - Latitude: 62.27 N - Longitude: 56.28 W..

1957 August 6 - . 15:30 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee. LV Configuration: Aerobee AC4.024.
  • Solar ultraviolet spectrum Solar ultraviolet mission - . Nation: USA. Agency: USAF. Apogee: 145 km (90 mi).

1957 August 6 - . 16:03 GMT - . Launch Site: Atlantic Ocean. Launch Pad: 63.9 N x 56.2 W. Launch Platform: LSD-29. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon II5.04F.
  • SUI 59 Ionosphere mission - . Nation: USA. Agency: SUI. Apogee: 117 km (72 mi). Summary: Launched at IGY Rockoon Launch Site 1, Atlantic Ocean LP4 - - Latitude: 63.93 N - Longitude: 56.15 W..

1958 August 6 - . LV Family: Saturn V. Launch Vehicle: Saturn V.
  • Rocketdyne gets F-1 engine contract. - . Nation: USA. Program: Apollo. Summary: Rocketdyne Division of North American announced an Air Force contract for a 1-million-pound thrust engine..

1958 August 6 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC18B. Launch Pad: LC18B. LV Family: Delta. Launch Vehicle: Thor DM-18. LV Configuration: Thor DM-18 117.
  • Research and development Series III test - . Nation: USA. Agency: USAF. Apogee: 520 km (320 mi).

1959 August 6 - .
  • F-102 for Mercury astronaut flight proficiency - . Nation: USA. Program: Mercury. Summary: Four F-102 aircraft were made available for use by the Mercury astronauts to maintain proficiency in high performance vehicles..

1959 August 6 - . 02:48 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Delta. Launch Vehicle: Thor DM-18A. LV Configuration: Thor DM-18A 208.
  • Series IV research and development launch - . Nation: USA. Agency: USAF. Apogee: 520 km (320 mi).

1960 August 6 - . 09:00 GMT - . Launch Site: Eglin. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun AA6.411.
  • Firefly GERTA Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 138 km (85 mi).

1961 August 6 - . 06:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Vostok 8K72K. LV Configuration: Vostok 8K72K E103-17.
  • Vostok 2 - . Call Sign: Oryel (Eagle ). Crew: Titov. Backup Crew: Nikolayev; Nelyubov. Payload: Vostok 3KA s/n 4. Mass: 4,730 kg (10,420 lb). Nation: USSR. Related Persons: Titov; Nikolayev; Nelyubov. Agency: RVSN. Program: Vostok. Class: Manned. Type: Manned spacecraft. Flight: Vostok 2. Spacecraft: Vostok. Duration: 1.00 days. Decay Date: 1961-08-07 . USAF Sat Cat: 168 . COSPAR: 1961-Tau-1. Apogee: 221 km (137 mi). Perigee: 172 km (106 mi). Inclination: 64.8000 deg. Period: 88.40 min. Second manned orbital flight. The Soviet Union successfully launched Vostok II into orbit with Gherman S. Titov as pilot. The spacecraft carried life-support equipment, radio and television for monitoring the condition of the cosmonaut, tape recorder, telemetry system, biological experiments, and automatic and manual control equipment. Flight objectives: Investigation of the effects on the human organism of a prolonged flight in orbit and subsequent return to the surface of the Earth; investigation of man's ability to work during a prolonged period of weightlessness. Titov took manual control of spacecraft but suffered from space sickness. He was equipped with a professional quality Konvas movie camera, with which ten minutes of film of the earth were taken through the porthole. Both television and film images were taken of the interior of the spacecraft. Like Gagarin, Titov experienced problems with separation of the service module after retrofire. Titov was never to fly again, after being assigned to the Spiral spaceplane, which turned out to be a dead-end project. A biography of him by Martin Caidin ('I Am Eagle') made him somewhat more accessible than Gagarin to the West.

1962 August 6 - .
  • MIT ordered Honeywell computer for work on the Apollo spacecraft navigation system - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Guidance. The MIT Instrumentation Laboratory ordered a Honeywell 1800 electronic computer from the Minneapolis- Honeywell Regulator Company's Electronic Data Processing Division for work on the Apollo spacecraft navigation system. After installation in 1963, the computer would aid in circuitry design of the Apollo spacecraft computer and would also simulate full operation of a spaceborne computer during ground tests.

1962 August 6 - .
1963 August 6 - . 06:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar Mayak-2. LV Family: Kosmos 2. Launch Vehicle: Kosmos 63S1.
  • Cosmos 19 - . Payload: DS-P1 s/n 3. Mass: 355 kg (782 lb). Nation: USSR. Agency: MO. Program: DS. Class: Military. Type: Military target satellite. Spacecraft: DS-P1. Completed Operations Date: 1964-03-29 . Decay Date: 1964-03-30 . USAF Sat Cat: 632 . COSPAR: 1963-033A. Apogee: 497 km (308 mi). Perigee: 267 km (165 mi). Inclination: 49.0000 deg. Period: 92.10 min. Summary: Prototype ABM radar target; supported developmental experiments for ABM systems..

1964 August 6 - . 16:30 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 628. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-7.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1964 August 6 - . 23:29 GMT - . Launch Site: Kronogard. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.55DA.
  • K64-S-1 Air sampling Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 125 km (77 mi).

1965 August 6 - . 17:41 GMT - . Launch Site: Delamar Dry Lake DZ. Launch Pad: 37.3 N x 114.9 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 1-56-93.
  • X-15A IR Scan,Stability test - . Nation: USA. Agency: NASA; USAF. Apogee: 31 km (19 mi). Summary: Maximum Speed - 5686 kph. Maximum Altitude - 31455 m..

1966 August 6 - . Launch Site: White Sands. LV Family: Apache. Launch Vehicle: Nike Apache.
  • Sphere Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1966 August 6 - . 06:30 GMT - . Launch Site: Kagoshima. LV Family: S. Launch Vehicle: S-210. LV Configuration: S-210 PT-210-1.
  • Test mission - . Nation: Japan. Agency: ISAS. Apogee: 1.00 km (0.60 mi).

1966 August 6 - . 08:00 GMT - . Launch Site: White Sands. LV Family: Apache. Launch Vehicle: Nike Apache.
  • Sphere Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1966 August 6 - . 11:00 GMT - . Launch Site: White Sands. LV Family: Apache. Launch Vehicle: Nike Apache.
  • Sphere Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1967 August 6 - . 04:04 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 5B. LV Configuration: Black Brant VB ALF-VB-13.
  • MPE Barium release Magnetosphere mission - . Nation: Germany. Agency: NRCC. Apogee: 287 km (178 mi).

1968 August 6 - . 01:55 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 5C. LV Configuration: Skylark-5C SL524.
  • Electron profile Ionosphere mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 234 km (145 mi).

1968 August 6 - . 11:16 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC13. LV Family: Atlas. Launch Vehicle: Atlas Agena D SLV-3A. LV Configuration: SLV-3A Agena D 5501A / Agena D 2801.
  • Canyon 1 - . Payload: Canyon 1 / Agena D / OPS 2222. Mass: 700 kg (1,540 lb). Nation: USA. Agency: NRO; USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Canyon. USAF Sat Cat: 3334 . COSPAR: 1968-063A. Apogee: 39,860 km (24,760 mi). Perigee: 31,680 km (19,680 mi). Inclination: 9.9000 deg. Period: 1,436.00 min. First launch in a communications intelligence program operated by the USAF within the National Reconnaissance Office, on behalf of the National Security Agency. The first generation series, CANYON, was based on the Agena vehicle. The Agena D remained attached to the spacecraft. Positioned in geosynchronous orbit over the Indian Ocean. Last known longitude (30 December 1968) 98.50 deg W drifting at 0.166 deg E per day.

1968 August 6 - . 16:33 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan 3B. LV Configuration: Titan IIIB 3B-17.
  • OPS 5187 - . Payload: KH-8 no. 15 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA. Agency: NRO; USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-8. Decay Date: 1968-08-16 . USAF Sat Cat: 3335 . COSPAR: 1968-064A. Apogee: 395 km (245 mi). Perigee: 142 km (88 mi). Inclination: 110.0000 deg. Period: 89.90 min. Summary: KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1968 August 6 - . 18:43 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 CRL AG3.532.
  • Extreme ultraviolet Mon / RPA Ionosphere / solar extreme ultraviolet mission - . Nation: USA. Agency: USAF. Apogee: 127 km (78 mi).

1969 August 6 - .
  • HL-10 Flight 23 - . Crew: Manke. Payload: HL-10 flight 23. Nation: USA. Related Persons: Manke. Program: NASA Lifting Body. Class: Manned. Type: Manned spaceplane. Spacecraft: HL-10. Summary: First 4-chambered flight. Maximum Speed - 1641 kph. Maximum Altitude - 23190 m. Flight Time - 372 sec..

1969 August 6 - . 05:40 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 291 - . Payload: IS-P Mass Model. Mass: 1,400 kg (3,000 lb). Nation: USSR. Agency: PKO. Class: Military. Type: Anti-satellite system target. Spacecraft: IS-P. Decay Date: 1969-09-08 . USAF Sat Cat: 4058 . COSPAR: 1969-066A. Apogee: 548 km (340 mi). Perigee: 144 km (89 mi). Inclination: 62.2000 deg. Period: 91.40 min. Summary: Test of Tsyklon 2 booster; ASAT target mass model. Did not enter typical target orbit due to lack of on-board engine. Simulated launch of ASAT interceptor planned for the next day was cancelled..

1970 August 6 - . 21:07 GMT - . Launch Site: Barking Sands. Launch Vehicle: Rocketsonde.
  • Met Para - . Nation: USA. Agency: MRN. Apogee: 54 km (33 mi).

1971 August 6 - . 12:50 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • OT GT85M operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1972 August 6 - . 14:00 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 89 km (55 mi).

1973 August 6 - . 00:08 GMT - . Launch Site: Kiruna. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.517UA.
  • SSC NNA 8 Aeronomy mission - . Nation: Sweden. Agency: NASA; SSC. Apogee: 103 km (64 mi).

1974 August 6 - . 00:02 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 670 - . Payload: Soyuz 7K-S s/n 1L. Mass: 6,700 kg (14,700 lb). Nation: USSR. Agency: MOM. Program: Salyut. Class: Manned. Type: Manned spacecraft. Spacecraft: Soyuz 7K-S. Duration: 2.99 days. Decay Date: 1974-08-09 . USAF Sat Cat: 7405 . COSPAR: 1974-061A. Apogee: 294 km (182 mi). Perigee: 211 km (131 mi). Inclination: 50.6000 deg. Period: 89.50 min. Summary: Unmanned Soyuz 7K-S test flight. Recovered August 8, 1974 23:59 GMT..

1975 August 6 - . 09:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 90 km (55 mi).

1976 August 6 - . 22:21 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan 34B. LV Configuration: Titan 34B 34B-6 (3B-56) / Ascent Agena D.
  • SDS no. 2 - . Payload: SDS no. 2 / OPS 7940. Mass: 700 kg (1,540 lb). Nation: USA. Agency: NRO; USAF. Class: Communications. Type: Military communications satellite. Spacecraft: SDS. USAF Sat Cat: 9270 . COSPAR: 1976-080A. Apogee: 39,315 km (24,429 mi). Perigee: 380 km (230 mi). Inclination: 63.3000 deg. Period: 703.80 min. Summary: Satellite Data Systems 2..

1977 August 6 - . 17:00 GMT - . Launch Site: Fort Sherman. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 64 km (39 mi).

1979 August 6 - .
  • Complete limit test (STA-099) - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Challenger. Summary: Complete limit test (STA-099), Lockheed facility, Palmdale.

1980 August 6 - . 01:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 78 km (48 mi).

1981 August 6 - . 08:16 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas Centaur SLV-3D. LV Configuration: SLV-3D Centaur AC-59 / Centaur D-1AR 5039. FAILURE: Failure of the fiberglass fairing during ascent.. Failed Stage: S.
  • Fltsatcom 5 - . Mass: 1,884 kg (4,153 lb). Nation: USA. Agency: USN. Class: Communications. Type: Military communications satellite. Spacecraft: Fltsatcom. Completed Operations Date: 1986-07-12 . USAF Sat Cat: 12635 . COSPAR: 1981-073A. Apogee: 36,300 km (22,500 mi). Perigee: 36,221 km (22,506 mi). Inclination: 8.9000 deg. Period: 1,460.40 min. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit. The Atlas G Centaur delivered a badly damaged but operating FLTSATCOM spacecraft to its correct orbit. Investigation showed that the most likely cause was failure of the fiberglass fairing during ascent. Positioned in geosynchronous orbit at 90 deg W in 1981; 90-114 deg W in 1982; 44 deg W in 1982-1986 As of 5 September 2001 located at 140.32 deg W drifting at 6.003 deg W per day. As of 2007 Mar 10 located at 31.85E drifting at 6.002W degrees per day.

1981 August 6 - . 11:49 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65055-112.
  • Cosmos 1287 - . Payload: Strela-1M no. 217. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 12636 . COSPAR: 1981-074A. Apogee: 1,513 km (940 mi). Perigee: 1,465 km (910 mi). Inclination: 74.0000 deg. Period: 115.70 min. Summary: Eight satellites launched by a single carrier rocket..
  • Cosmos 1294 - . Payload: Strela-1M no. 224. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 12643 . COSPAR: 1981-074H. Apogee: 1,465 km (910 mi). Perigee: 1,392 km (864 mi). Inclination: 74.0000 deg. Period: 114.40 min.
  • Cosmos 1292 - . Payload: Strela-1M no. 222. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 12641 . COSPAR: 1981-074F. Apogee: 1,477 km (917 mi). Perigee: 1,464 km (909 mi). Inclination: 74.0000 deg. Period: 115.30 min.
  • Cosmos 1290 - . Payload: Strela-1M no. 220. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 12639 . COSPAR: 1981-074D. Apogee: 1,465 km (910 mi). Perigee: 1,442 km (896 mi). Inclination: 74.0000 deg. Period: 115.00 min.
  • Cosmos 1291 - . Payload: Strela-1M no. 221. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 12640 . COSPAR: 1981-074E. Apogee: 1,465 km (910 mi). Perigee: 1,458 km (905 mi). Inclination: 74.0000 deg. Period: 115.10 min.
  • Cosmos 1289 - . Payload: Strela-1M no. 219. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 12638 . COSPAR: 1981-074C. Apogee: 1,465 km (910 mi). Perigee: 1,426 km (886 mi). Inclination: 74.0000 deg. Period: 114.80 min.
  • Cosmos 1288 - . Payload: Strela-1M no. 218. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 12637 . COSPAR: 1981-074B. Apogee: 1,492 km (927 mi). Perigee: 1,465 km (910 mi). Inclination: 74.0000 deg. Period: 115.50 min.
  • Cosmos 1293 - . Payload: Strela-1M no. 223. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 12642 . COSPAR: 1981-074G. Apogee: 1,465 km (910 mi). Perigee: 1,409 km (875 mi). Inclination: 74.0000 deg. Period: 114.60 min.

1982 August 6 - . 14:20 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 90 km (55 mi).

1983 August 6 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 641. LV Family: Trident. Launch Vehicle: Trident C-4.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1983 August 6 - . 00:38 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 641. LV Family: Trident. Launch Vehicle: Trident C-4.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1984 August 6 - . 14:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1587 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 25.00 days. Decay Date: 1984-08-31 . USAF Sat Cat: 15163 . COSPAR: 1984-082A. Apogee: 365 km (226 mi). Perigee: 194 km (120 mi). Inclination: 72.9000 deg. Period: 90.10 min. Summary: Military cartographic satellite; returned film capsule. Return date suspect..

1985 August 6 - . 20:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 93 km (57 mi).

1985 August 6 - .
1986 August 6 - . 13:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2.
  • Cosmos 1770 - . Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4KS1. Duration: 180.00 days. Decay Date: 1987-02-02 . USAF Sat Cat: 16897 . COSPAR: 1986-060A. Apogee: 292 km (181 mi). Perigee: 234 km (145 mi). Inclination: 64.7000 deg. Period: 89.80 min. Summary: Photo/digital surveillance..

1987 August 6 - . 21:49 GMT - . Launch Site: Barking Sands. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 69 km (42 mi).

1988 August 6 - .
  • Cosmonaut Anatoli Semyonovich Levchenko dies at age of 47 -- Natural causes - Brain tumor - at Nikolai Burdenko Neurosurgical Institute in Moscow. - . Nation: USSR. Related Persons: Levchenko. Summary: Ukrainian test pilot cosmonaut. Flew on Mir LII-1. Graduated from Chernigov Higher Air Force School, 1964. Buran test pilot; cosmonaut training December 1978 - July 1980. Later a civil test pilot for the Soviet Air Force Ministry..

1992 August 6 - . 19:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-ML.
  • Molniya 1-84 - . Payload: Molniya-1T. Mass: 1,600 kg (3,500 lb). Nation: Russia. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-1T. Decay Date: 2008-04-04 . USAF Sat Cat: 22068 . COSPAR: 1992-050A. Apogee: 39,294 km (24,416 mi). Perigee: 1,060 km (650 mi). Inclination: 63.0000 deg. Period: 717.80 min. Summary: Operation of the long-range telephone and telegraph radio communications system, transmission of television programmes to stations in the Orbita network. .

1993 August 6 - .
  • Death of Milton Orville 'Milt' Thompson at Lancaster, California. Natural causes. - . Nation: USA. Related Persons: Thompson. Summary: American test pilot astronaut, 1962-1963. Flew lifting bodies, X-15, assigned as X-20 spaceplane astronaut..

1996 August 6 - . LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Endeavour OMDP-1 - . Nation: USA. Program: STS. Spacecraft: Endeavour. Summary: Shuttle Endeavour undergoes its OMDP-1 Orbiter Maintenance Down Period at Palmdale, returning to service on 4 April 1997. These overhauls are undertaken every 10 to 12 shuttle missions..

1997 August 6 - .
  • Mir News 375: Soyuz-TM26 - . Nation: Russia. Program: Mir. Flight: Mir EO-24; Mir NASA-4; Mir EO-23. The perfect launch took place on 5.08.1997 at 15.35.59 UTC. On board the crew for the 24th Main Exp. to Mir, Anatoliy Solovyov and Pavel Vinogradov . Call sign: Rodniki, so Rodnik-1 and Rodnik-2. During the first pass in orb. 2 (1838-1841 UTC) very weak signals on beacon- and telephony frequencies. During the pass in orb. 3 (2007-2011 UTC) very good reception on all frequencies. Solovyov could be heard in a conversation with TsUP. He reported a technical anomaly in the BO (life compartment): a hose (or: tube) was not connected to an air purification unit, which caused an increased amount of CO2 in the mini-atmosphere on board. He told TsUP that he had connected that hose immediately and that the system was functioning normally. Again good signals in the window in orb. 4 (2138-2147 UTC) during which Solovyev repeated his report about that hose.

    Mir:

    During the passes in the evening of 4.08.1997 the crew reported that they were working on the malfunctioning Elektron oxygen generator in Kvant-1. (The Elektron in Kvant-2 is not operational due to power shortages). During a long communication session via Altair-2 in the morning of 5.08.1997 the crew was still co-ordinating the repair work on the Elektron. After the departure of Progress-M35 for a 10 day lasting autonomous flight lithium perchlorate cartridges have to be used for the production of oxygen. This will be not very convenient during the period in which 5 men are on board (7-14.08.97).

    An eventual delay of the Soyuz-TM26 launch due to the problems with the Elektrons has not been taken into consideration.

    In MirNEWS.374 I gave an estimated time for the docking of Soyuz-TM26 on 7.08.97 as 1723 UTC. In that report I remarked that this time considerably deviated from the normal routine: dockings a few minutes after LOS of the first pass of both objects for our position. Inquiries in the Ballistic Section of the Keldysh institute of the R.A.N. learned that there had been a misprint in a Russian message about the estimated docking time. The estimated docking time is: 07.08.97 at 1703 UTC, so in accordance with the normal routine.

    The supply ship Progress-M35 has to free the docking port (+X-axis) for the arrival of the Soyuz-TM26 and will do this on 6.08.97 at 1144 UTC. The autonomous flight of Progress-M35 will last until 16.08.97. On that day Progress-M35 will dock (in the automatic regime with the system Kurs) at the same docking port after the redocking of Soyuz-TM26 to the forward (-X-axis) the day before. Chris v.d. Berg, NL-9165/A-UK3202.


2000 August 6 - . 18:26 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U K15000-668.
  • Progress M1-3 - . Payload: Progress M1 s/n 251. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RAKA. Manufacturer: Korolev. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: STS-106. Spacecraft: Progress M1. Duration: 86.53 days. Decay Date: 2000-11-01 . USAF Sat Cat: 26461 . COSPAR: 2000-044A. Apogee: 362 km (224 mi). Perigee: 347 km (215 mi). Inclination: 51.5000 deg. Period: 91.63 min. Progress M1-3 automatically docked with the International Space Station on August 8 at 20:13 GMT at the rear Zvezda port. The supply ship began refuelling of the station a few days later. It remained attached for offloading of its dry cargo by the STS-106 crew. It later separated from Zvezda's rear port at 0405 GMT November 1 and was deorbited over the Pacific at 0705 GMT.

2001 August 6 - .
  • Galileo, Io 31 Flyby - . Nation: USA. Spacecraft: Galileo.

2001 August 6 - . 07:28 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Titan. Launch Vehicle: Titan 402B/IUS. LV Configuration: Titan 402B 4B-31 / IUS.
  • USA 159 - . Payload: DSP-1 Block 18 F21. Mass: 2,380 kg (5,240 lb). Nation: USA. Agency: USAF. Manufacturer: TRW. Class: Military. Type: Early warning satellite. Spacecraft: DSP. USAF Sat Cat: 26880 . COSPAR: 2001-033A. Apogee: 35,780 km (22,230 mi). Perigee: 35,780 km (22,230 mi). Inclination: 2.9000 deg. Period: 1,435.76 min. Launch postponed from February, then delayed from July 27. USA 159 was a US Air Force Defense Support Program infrared missile early warning satellite was placed by the Titan core into a 328 x 663 km x 28.7 deg parking orbit. The Boeing IUS-16 upper stage then fired its first solid motor to enter geostationary transfer orbit. The second IUS solid motor fired at around 14:00 GMT placing DSP Flight 21 in near-geosynchronous orbit. Still in service as of March 2007.

2002 August 6 - . 18:30 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.202US.
  • USC-4 (SOHO SEM) Solar extreme ultraviolet mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

2003 August 6 - . 09:06 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 GT183GB.
  • GT183GB Functional Dependency gate operational test launch - . Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi).

2004 August 6 - .
  • International Space Station Status Report #04-44 - . Nation: USA. Related Persons: Fincke; Padalka. Program: ISS. Flight: ISS EO-9. Aboard the International Space Station this week, Expedition 9 Commander Gennady Padalka and NASA ISS Science Officer Mike Fincke resumed scientific investigations, routine maintenance, and preparations for the arrival of a new cargo ship - all following a spacewalk on Tuesday. Additional Details: International Space Station Status Report #04-44.

2005 August 6 - .
2007 August 6 - . 22:56 GMT - . Launch Site: Andoya. LV Family: Terrier. Launch Vehicle: Terrier Orion Improved. LV Configuration: Terrier Improved Orion NASA 41.070.
  • MASS 2 (NLCs) Aeronomy mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 130 km (80 mi).

2010 August 6 - . 15:15 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: Tula. LV Family: R-29. Launch Vehicle: Sineva.
  • RV x4 - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Operational test..

2010 August 6 - . 15:15 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: Tula. LV Family: R-29. Launch Vehicle: Sineva.
  • RV x4 - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Operational test..

2011 August 6 - . 22:52 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Astra 1N - . Nation: Luxembourg. Program: Astra. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 37775 . COSPAR: 2011-041A. Apogee: 35,802 km (22,246 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.0000 deg. Period: 1,436.00 min. Summary: Geosynchronous communications satellite to be stationed at 19.2 deg E for direct television broadcasting to Europe..
  • BSAT-3C - . Payload: A2100A. Nation: Japan. Program: BSAT. Class: Communications. Type: Communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 37776 . COSPAR: 2011-041B. Apogee: 35,791 km (22,239 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Japan's Broadcast Satellite Systems Corporation communications satellite..

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