WS 107A-1Flight Test Working Group Flight Test Report Atlas Missile 4 F, 23 November 1961, AMR Range Test Number 3751 Astronautics Test Number P1-601-00-4
WS 107A-1Flight Test Working Group Flight Test Report Atlas Missile 4 F, 23 November 1961, AMR Range Test Number 3751 Astronautics Test Number P1-601-00-4
The primary purposes of this flight were to obtain data on the re-entry vehicle impact location for the statistical determination of the CEP, to evaluate the ability of the MAPCHE System and procedures to check out a missile and place it in a first readiness condition, to evaluate the Sandia simulated warhead, to evaluate the Acoustica PU System, and to evaluate the Inertial Guidance System performance and accuracy. (Author)
Document information
WS 107A-1Flight Test Working Group Flight Test Report Atlas Missile 4 F, 23 November 1961, AMR Range Test Number 3751 Astronautics Test Number P1-601-00-4
1961
87 pages
Report
No indication
English
Missile Technology , Surface to surface missiles , Flight testing , Reentry vehicles , Impact prediction , Circular error probable , Checkout equipment , Ground support equipment , Guided missile warheads , Propellant control , Inertial guidance , Miss distance , Airframes , Liquid propellant rocket engines , Pneumatic devices , Hydraulic equipment , Guided missile tracking systems , Telemeter systems , Transponders , Flight control systems , Atlas , Azusa , Mark-5 reentry vehicles , Xsm-65f missiles