WS 107-1Flight Test Working Group, Flight Test Report, Atlas Missile 26E
WS 107-1Flight Test Working Group, Flight Test Report, Atlas Missile 26E
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)
Dokumentinformationen
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