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)
Flight Test Report Atlas Missile 16E, 24 March 1961
1961
82 pages
Report
Keine Angabe
Englisch
Missile Technology , Surface to surface missiles , Flight testing , Inertial guidance , Guided missile warheads , Arming devices , Range(Distance) , Failure , Miss distance , Booster rockets , Jettisonable equipment , Electrical equipment , Vernier rocket engines , Pneumatic devices , Telemeter systems , Airframes , Beacons , Hydraulic equipment , Guided missile tracking systems , Flight control systems , Transponders , Reentry vehicles , Atmosphere entry , Atlas , Azusa , Xsm-65e missiles
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