Mercury Booster Working Group Flight Test Report Mercury/Atlas MA-3 (Atlas 100D) 25 April 1961.

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Abstract:

The report describes the launch and flight parameters of an unmanned spacecraft.

Author(s):
No Author(s) Identified
Author Organization(s):
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Pagination:
0067

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
GDA-AA61-0057
 Subject Terms
Communities of Interest:
Space
Descriptor(s):
(*LAUNCH VEHICLES, FLIGHT TESTING), LAUNCHING SITES, GUIDED MISSILE TRAJECTORIES, ASCENT TRAJECTORIES, GUIDED MISSILE LAUNCHERS, GUIDED MISSILE COMPUTERS, AUTOMATIC PILOTS, FAILURE, GUIDED MISSILE SAFETY, PERFORMANCE(ENGINEERING), RELIABILITY(ELECTRONICS), DESTRUCTORS
Field(s)/Group(s):
Spacecraft Trajectories and Reentry, Ground Support Systems and Facilities for Space Vehicles
Keyword(s):
ATLAS LAUNCH VEHICLES, MA 3 PROPULSION SYSTEMS, MERCURY PROJECT
Report Date:
1961 May 08