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USAF OAR
Country: USA.
1965 October 5 - . 09:07 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D.
- 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: 144.20 deg. Period: 117.60 min. 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.
- 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: 144.50 deg. Period: 104.00 min. 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: 144.60 deg. Period: 105.60 min. 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.
- 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: 82.40 deg. Period: 126.40 min. 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.
- 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: 40.90 deg. Period: 142.90 min. 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. 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: 144.20 deg. Period: 105.20 min. 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.
- 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: 81.40 deg. Period: 121.40 min. 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.
- 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: 81.90 deg. Period: 104.20 min. 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.
- 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: 99.10 deg. Period: 139.40 min. 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: 93.40 deg. Period: 96.10 min. 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. 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: 101.60 deg. Period: 95.50 min. 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: 101.70 deg. Period: 95.40 min. 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.
- 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: 90.00 deg. Period: 93.00 min. 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.
- 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: 100.00 deg. Period: 198.70 min. 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: 100.00 deg. Period: 207.00 min. 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.
- 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: 89.80 deg. Period: 104.60 min. 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: 89.80 deg. Period: 91.50 min. 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.
- 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: 99.10 deg. Period: 93.20 min.
Atlas 104F was launched from Vandenberg AFB and placed 41 scientific experiments into orbit as part of SAMSO's Space Experiments Support Program (SESP). Solar radiation experiments. 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: 98.90 deg. Period: 95.20 min. 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: 104.80 deg. Period: 151.10 min. 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: 99.10 deg. Period: 89.40 min. Radio beacon mountedon OV17 propulsion module. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
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