The primary purposes of the flight were to obtain data for statistical determination of CEP, evaluate the performance of the Acoustica PU system and to determine re-entry vehicle structural capabilities at high angle re-entry conditions. (Author)
WS 107-1Flight Test Working Group, Flight Test Report, Atlas Missile 26E
1961
75 pages
Report
Keine Angabe
Englisch
Missile Technology , Surface to surface missiles , Flight testing , Miss distance , Reentry vehicles , Atmosphere entry , Sustainer engines , Booster rockets , Abort , Propellant control , Circular error probable , Impact prediction , Pneumatic devices , Hydraulic equipment , Telemeter systems , Descent trajectories , Guided missile tracking systems , Flight control systems , Inertial guidance , Atlas , Azusa , Xsm-65e missiles