Launch Success
Liftoff Time (GMT)
16:36:00
Wednesday February 3, 1965
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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 entire celestial sphere for direction and intensity of UV light and X-ray and gamma radiation. The OSO 2 platform consisted of a sail section, which pointed two experiments continuously toward the sun, and a wheel section, which spun about an axis perpendicular to the pointing direction of the sail and carried six experiments. Attitude adjustment was performed by gas jets.
Low Earth Orbit
1 Payload
547 kilograms


Agency
US Air ForceRocket
Height: 31m
Payload to Orbit
LEO: 410 kg
GTO: 82 kg
Liftoff Thrust
667 Kilonewtons
Stages
3
5th
Mission
2nd
Mission of 1965
8th
Orbital launch attempt