Atlas-OIS
Description
The Atlas E/F (or SB-1A) was an American expendable launch system built using parts of decommissioned SM-65 Atlas missiles. The OIS upper stage was used for two Atlas E/F launches.
Missions
2
Success Rate
100.0%
Successes
2
Failures
0
Success Streak
2
Partial Failures
0
Previous
March 13, 1985
Geosat
Atlas-E/F OIS | General Dynamics
Vandenberg SFB, California, USA
February 24, 1979
Solwind
Atlas-E/F OIS | General Dynamics
Vandenberg SFB, California, USA
Configurations
Retired
Atlas-E/F OIS
Active 1979 to 1985
Payload to Orbit
LEO: 870 kg
Stages
2