The primary purposes of the flight were to obtain data for determining the performance of the Propellant Utilization System and to evaluate the Inertial Guidance System Performance. (Author)
WS 107A-1Flight Test Working Group, Flight Test Report, Atlas Missile 32E
1961
69 pages
Report
No indication
English
Missile Technology , Surface to surface missiles , Flight testing , Inertial guidance , Liquid propellant rocket engines , Sustainer engines , Failure , Destructors , Abort , Liquid rocket oxidizers , Flight control systems , Propellant control , Pressure regulators , Telemeter systems , Pneumatic devices , Hydraulic equipment , Atlas , Azusa , Xsm-65e missiles