This report defines the flight performance of a guided missile. The primary purposes of this flight were to determine the performance of the re-entry vehicle, with principle emphasis on the operation of the simulated war-head, and to evaluate the guidance system accuracy. Detailed objectives are listed along with comments on the degree to which they were satisfied. (Author)
Flight Test Working Group. Flight Test Report Atlas Missile 62D 22 June 1960, Ws 107A-1
1960
85 pages
Report
No indication
English
Missile Technology , Surface to surface missiles , Flight testing , Liquid propellant rocket engines , Propellant tanks , Propellant control , Pneumatic devices , Electrical equipment , Guided missile safety , Telemeter systems , Inertial guidance , Flight control systems , Impact prediction , Reentry vehicles , Propellant transfer , Ground support equipment , Performance(Engineering) , Reliability(Electronics) , Atlas , Xsm-65d missiles