Encyclopedia Astronautica
USAF OAR


American agency. USAF OAR, USA.

AKA: USAF.

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  • Agency Agencies or institutions overseeing design, development, construction, or operation of space-related systems. More...

USAF OAR Chronology


1965 October 5 - . 09:07 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 34D NB20.170 RS.
  • OV1-02 - . Payload: OV1 Dummy. Mass: 86 kg (189 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. USAF Sat Cat: 1613 . COSPAR: 1965-078A. Apogee: 2,735 km (1,699 mi). Perigee: 408 km (253 mi). Inclination: 144.2000 deg. Period: 117.60 min. Summary: Radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1966 March 30 - . 09:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 72D NB20.152 RS.
  • OV1-04 - . Mass: 88 kg (194 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. USAF Sat Cat: 2121 . COSPAR: 1966-025A. Apogee: 1,008 km (626 mi). Perigee: 884 km (549 mi). Inclination: 144.5000 deg. Period: 104.00 min. Summary: Thermal control experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OV1-05S - . Payload: BORE. Mass: 114 kg (251 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. USAF Sat Cat: 2122 . COSPAR: 1966-025B. Apogee: 1,056 km (656 mi). Perigee: 985 km (612 mi). Inclination: 144.6000 deg. Period: 105.60 min. Summary: Optical radiation test. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1966 April 22 - . 09:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout B. LV Configuration: Scout B S145C.
  • OV3-01 - . Mass: 69 kg (152 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV3. USAF Sat Cat: 2150 . COSPAR: 1966-034A. Apogee: 3,585 km (2,227 mi). Perigee: 341 km (211 mi). Inclination: 82.4000 deg. Period: 126.40 min. Summary: Radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..

1966 June 10 - . 04:15 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA3A. LV Family: Scout. Launch Vehicle: Scout B. LV Configuration: Scout B S147C.
  • OV3-04 - . Mass: 79 kg (174 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV3. USAF Sat Cat: 2201 . COSPAR: 1966-052A. Apogee: 4,704 km (2,922 mi). Perigee: 643 km (399 mi). Inclination: 40.9000 deg. Period: 142.90 min. Summary: Radiation measurements. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1966 July 14 - . 02:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 58D. FAILURE: Partial Failure.. Failed Stage: 1.
  • OV1-07 - . Payload: PasComSat. Mass: 10 kg (22 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1978-01-04 . USAF Sat Cat: 2324 . COSPAR: 1966-063A. Apogee: 1,022 km (635 mi). Perigee: 985 km (612 mi). Inclination: 144.2000 deg. Period: 105.20 min. Summary: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1966 August 4 - . 10:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout B. LV Configuration: Scout B S148C.
  • OV3-03 - . Mass: 75 kg (165 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV3. USAF Sat Cat: 2389 . COSPAR: 1966-070A. Apogee: 3,141 km (1,951 mi). Perigee: 349 km (216 mi). Inclination: 81.4000 deg. Period: 121.40 min. Summary: Radiation measurements. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1966 October 28 - . 11:56 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout B. LV Configuration: Scout B S150C.
  • OV3-02 - . Mass: 82 kg (180 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV3. Decay Date: 1971-09-29 . USAF Sat Cat: 2517 . COSPAR: 1966-097A. Apogee: 1,599 km (993 mi). Perigee: 319 km (198 mi). Inclination: 81.9000 deg. Period: 104.20 min. Summary: Radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1966 December 11 - . 21:09 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 89D / OV-1 (2x).
  • OV1-09 - . Mass: 230 kg (500 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. USAF Sat Cat: 2610 . COSPAR: 1966-111A. Apogee: 4,582 km (2,847 mi). Perigee: 475 km (295 mi). Inclination: 99.1000 deg. Period: 139.40 min. Summary: Radiation bio-hazard experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OV1-10 - . Mass: 130 kg (280 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 2002-11-30 . USAF Sat Cat: 2611 . COSPAR: 1966-111B. Apogee: 604 km (375 mi). Perigee: 541 km (336 mi). Inclination: 93.4000 deg. Period: 96.10 min. Summary: Radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1967 July 27 - . 19:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 92D. FAILURE: Partial Failure.. Failed Stage: 1.
  • OV1-08S - . Mass: 118 kg (260 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1972-02-22 . USAF Sat Cat: 2893 . COSPAR: 1967-072A. Apogee: 557 km (346 mi). Perigee: 529 km (328 mi). Inclination: 101.6000 deg. Period: 95.50 min. Summary: Carried cosmic ray telescope. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OV1-12S - . Mass: 140 kg (300 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1980-07-22 . USAF Sat Cat: 2901 . COSPAR: 1967-072D. Apogee: 579 km (359 mi). Perigee: 497 km (308 mi). Inclination: 101.7000 deg. Period: 95.40 min. Summary: Solar flare observations. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1967 December 5 - . 01:03 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout B. LV Configuration: Scout B S158C.
  • OV3-06 - . Payload: ATCOS 2. Mass: 95 kg (209 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV3. Decay Date: 1969-03-09 . USAF Sat Cat: 3057 . COSPAR: 1967-120A. Apogee: 443 km (275 mi). Perigee: 409 km (254 mi). Inclination: 90.0000 deg. Period: 93.00 min. Summary: Ionospheric studies. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1968 April 6 - . 09:59 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 107F / OV-1 (2x).
  • OV1-13 - . Mass: 107 kg (235 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. USAF Sat Cat: 3173 . COSPAR: 1968-026A. Apogee: 9,214 km (5,725 mi). Perigee: 587 km (364 mi). Inclination: 100.0000 deg. Period: 198.70 min. Summary: Radiation, engineering experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OV1-14 - . Mass: 101 kg (222 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. USAF Sat Cat: 3174 . COSPAR: 1968-026B. Apogee: 9,858 km (6,125 mi). Perigee: 568 km (352 mi). Inclination: 100.0000 deg. Period: 207.00 min. Summary: Radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1968 July 11 - . 19:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 75F / OV-1 (2x).
  • OV1-15S - . Payload: Spades. Mass: 470 kg (1,030 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1968-11-06 . USAF Sat Cat: 3318 . COSPAR: 1968-059A. Apogee: 1,800 km (1,100 mi). Perigee: 153 km (95 mi). Inclination: 89.8000 deg. Period: 104.60 min. Summary: Studied relationship between atmospheric density and solar radiation. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OV1-16 Cannonball 1 - . Payload: Loads. Mass: 600 kg (1,320 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1968-08-19 . USAF Sat Cat: 3319 . COSPAR: 1968-059B. Apogee: 556 km (345 mi). Perigee: 145 km (90 mi). Inclination: 89.8000 deg. Period: 91.50 min. Summary: Ionospheric drag tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1969 March 18 - . 07:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 104F / OV-1 (3x).
  • OV1-17S - . Mass: 142 kg (313 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1970-03-05 . USAF Sat Cat: 3823 . COSPAR: 1969-025A. Apogee: 466 km (289 mi). Perigee: 400 km (240 mi). Inclination: 99.1000 deg. Period: 93.20 min. Summary: Solar radiation experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OV1-17A Orbiscal 2 - . Payload: OV1-17P. Mass: 221 kg (487 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1969-03-24 . USAF Sat Cat: 3826 . COSPAR: 1969-025D. Apogee: 309 km (192 mi). Perigee: 175 km (108 mi). Inclination: 99.1000 deg. Period: 89.40 min. Summary: Radio beacon mountedon OV17 propulsion module. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OV1-18S - . Mass: 125 kg (275 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1972-08-27 . USAF Sat Cat: 3824 . COSPAR: 1969-025B. Apogee: 583 km (362 mi). Perigee: 466 km (289 mi). Inclination: 98.9000 deg. Period: 95.20 min. Summary: Ionospheric, radiation, electric field data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OV1-19S - . Mass: 124 kg (273 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. USAF Sat Cat: 3825 . COSPAR: 1969-025C. Apogee: 5,551 km (3,449 mi). Perigee: 483 km (300 mi). Inclination: 104.8000 deg. Period: 151.10 min. Summary: Radiation experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

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