The primary purposes of this flight were to determine missile system extended range capability, evaluate guidance system performance and accuracy, determine performance of the Mark 3 Mod 1B re-entry vehicle, and determine the performance of the arming and fuzing system. (Author)
Flight Test Report Atlas Missile 17E 22 June 1961
1961
82 pages
Report
Keine Angabe
Englisch
Missile Technology , Surface to surface missiles , Flight testing , Inertial guidance , Range(Distance) , Reentry vehicles , Atmosphere entry , Separation , Arming devices , Destructors , Liquid propellant rocket engines , Pneumatic devices , Hydraulic equipment , Telemeter systems , Guided missile tracking systems , Transponders , Flight control systems , Propellant control , Propellant transfer , Atlas , Azusa , Mark-3 reentry vehicles , Xsm-65e missiles
Flight Test Report Atlas Missile 71D
NTIS | 1960
Atlas/Agena Flight Test Directive Atlas Missile 118D
NTIS | 1962
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