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MA-1 (8)

Mercury-Atlas 1
Pad LC-14 ()
Atlas (1)

Crew: Unmanned

Milestones: n/a

Payload: Spacecraft No. 4, Launch Vehicle 50-D

Mission Objective:  

Qualify Spacecraft and Atlas combination. The specific test objectives were,

1. Recover the capsule,
2. Determine the structural integrity of the Mercury capsule structure and afterbody shingles under the maximum heating conditions which could be encountered from an orbital launching. 
3. Determine Mercury capsule afterbody heating rates during reentry (for this purpose 51 thermocouples were installed).
4. Determine the flight dynamic characteristics of the Mercury capsule during reentry.
5. Determine the adequacy of the Mercury capsule recovery systems.
6. Familiarize Project Mercury operating personnel with launch and recovery operations.

Orbit:

Altitude: 8.1 statute miles
Orbits: 0
Duration: Days, hours, min, seconds
Distance: 6 statute miles
Velocity: 1,701 mph

Launch: July 29, 1960


Landing: n/a


Mission Highlights: Mission listed as a failure

 

Page Last Revised

Page & Curator Information

09/29/2000

Curator: Kay Grinter (kay.grinter@jbosc.ksc.nasa.gov)
Web Development: JBOSC Web Development Team
A Service of the NASA/KSC External Relations and Business Development Directorate
JoAnn H. Morgan, Director