WS 107A-1Flight Test Working Group Flight Test Report Atlas Missile 35E, 1 December 1961, AMR Range Test Number 5462 Astronautics Test Number P3-501-00-35
WS 107A-1Flight Test Working Group Flight Test Report Atlas Missile 35E, 1 December 1961, AMR Range Test Number 5462 Astronautics Test Number P3-501-00-35
The primary purposes of this flight were to obtain data on the location of the re-entry vehicle impact for the statistical determination of the CEP, to determine re-entry vehicle and missile system compatibility, to evaluate the Inertial Guidance System performance, to evaluate the performance of the Acoustica PU System and to determine the open loop performance of the tank fragmentation system. (Author)
Document information
WS 107A-1Flight Test Working Group Flight Test Report Atlas Missile 35E, 1 December 1961, AMR Range Test Number 5462 Astronautics Test Number P3-501-00-35
1961
88 pages
Report
No indication
English
Missile Technology , Surface to surface missiles , Flight testing , Impact prediction , Circular error probable , Reentry vehicles , Propellant control , Miss distance , Telemeter systems , Airframes , Liquid propellant rocket engines , Pneumatic devices , Hydraulic equipment , Guided missile ranges , Guided missile tracking systems , Transponders , Flight control systems , Inertial guidance , Atlas , Azusa , Mark-4 reentry vehicles , Open loop control systems , Xsm-65e missiles