Atlas-OV1
Description
The Atlas E/F (or SB-1A) was an American expendable launch system built using parts of decommissioned SM-65 Atlas missiles. The Atlas E/F was used between 1968 and 1971 to launch OV1 satellites, using OV1 upper stages. Each payload had its own upper stage.
Missions
11
Success Rate
72.7%
Successes
7
Failures
2
Success Streak
4
Partial Failures
2
Previous
August 7, 1971
OV1-20 OV1-21
Atlas-E/F OV1 | General Dynamics
Vandenberg SFB, California, USA
March 18, 1969
OV1-17/OV1-18/OV1-19
Atlas-E/F OV1 | General Dynamics
Vandenberg SFB, California, USA
Configurations
Retired
Atlas-E/F OV1
Active 1968 to 1971
Payload to Orbit
LEO: 363 kg
Stages
2
Retired
Atlas-D OV1
Active 1965 to 1967
Liftoff Thrust
1,880 Kilonewtons
Stages
2