The most significant Atlas weapon system objective for this flight was to obtain data for the statistical determination of the circular error probable. (Author)
WS 107A-1Flight Test Working Group Flight Test Report Atlas Missile 2F
1961
81 pages
Report
Keine Angabe
Englisch
Missile Technology , Surface to surface missiles , Flight testing , Reentry vehicles , Miss distance , Propellant control , Gyro stabilizers , Aerodynamic characteristics , Circular error probable , Airframes , Liquid propellant rocket engines , Pneumatic devices , Hydraulic equipment , Flight control systems , Inertial guidance , Guided missile tracking systems , Telemeter systems , Transponders , Decoys , Atlas , Azusa , Closed loop systems , Control , Control systems , Mark-5 reentry vehicles , Xsm-65f missiles