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Object Name | OSO 1 |
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Object Full Name | - |
Norad ID | 255 |
Cospar ID | 1962-006A |
Object Type | Satellite |
Object Status | Decayed |
Object Class | - |
End of Life | - |
The objectives of the OSO satellite series were to perform solar physics experiments above the atmosphere during a complete solar cycle and to map the celestial sphere for direction and intensity of UV light, X-rays, and gamma radiation. The OSO 1 was the first satellite to have pointed instruments and onboard tape recorders for data storage. The OSO 1 platform consisted of a sail section, which pointed two experiments continuously toward the sun, supplying power to the experiments from the solar batteries and rechargeable chemical batteries; and a wheel section, which spun about an axis perpendicular to the pointing direction of the sail and carried seven experiments. Attitude adjustment was performed by gas jets. Data were simultaneously recorded on tape and transmitted by FM telemetry. A command system provided for 10 ground-based commands. The spacecraft performed normally until the second onboard tape recorder failed May 15, 1962. The spacecraft provided real-time data until May 1964, when the power cells failed. For more information, see A. W. L. Ball, Spaceflight, v. 12, p. 244, 1970.
Launch Date | 1962-03-07 |
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Decay Date | 1981-10-08 |
Launch Vehicle | - |
Launch Site | Air Force Eastern Test Range, Florida, USA |
Launch Provider | - |
Launch Provider Country | - |
Launch Mass | - |
Dry Mass | - |
User | - |
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Mission | - |
Mission Detail | - |
Country of Registry | - |
Programme | - |
Operator | - |
Country of Operator | United States |
Contractor | - |
Country of Contractor | - |
Payload Contractor | - |
Payload Contractor Country | - |
Orbit Status | Earth Orbit |
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Orbit | - |
Orbit Type | - |
Period: | 87.4 min |
Inclination: | 32.8° |
Apogee: | 147.0 km |
Perigee: | 147.0 km |
Longitude of Geo | - |
ECT | - |
Payload | - |
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Platform | - |
Propulsion | - |
Propulsion Type | - |
Life Time | - |
Power | - |
Budget | - |
Call Sign | - |
Beacon | - |
RCS | 1.7300 m² |
References | - |
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Angular Momentum: | - |
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Eccentricity: | - |
Inclination: | - |
RAAN: | - |
Argument of Perigee: | - |
True Anomaly: | - |
Period: | - |
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Semi-Major Axis: | - |
Perigee: | - |
Apogee: | - |
Mean Motion: | - |
Mean Anomaly: | - |
Latitude: | - |
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Longitude: | - |
Altitude: | - |
Speed: | - |
Azimuth: | - |
Elevation: | - |
Range: | - |