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Accession Number:
AD0843410
Title:
Flight Test Report Atlas Missile 16E, 24 March 1961.
Corporate Author:
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Report Date:
1961-04-06
Abstract:
The primary purpose of the flight was to evaluate E series missile system performance at maximum R and D range. Other first order objectives included evaluation of Inertial Guidance System performance and accuracy, determination of warhead performance, arming and fuzing system performance, and missile system maximum range capability. Author
Pages:
0082
File Size:
0.00MB
