This was the second flight test of the 'E' Series airframe and MA-3 propulsion system and provided for continued testing of the ARMA All Inertial Guidance System and for impact data for CEP determination. The results of these and other flight test objectives are presented, along with comments relative to the degree of satisfaction. Premature flight termination precluded satisfying many of the objectives. (Author)
WS 107A-1Flight Test Working Group Flight Test Report, ATLAS Missile 4E, 20 November 1960
1960
80 pages
Report
Keine Angabe
Englisch
Missile Technology , Surface to surface missiles , Flight testing , Miss distance , Sustainer engines , Hydraulic equipment , Thrust , Failure , Vernier rocket engines , Telemeter systems , Liquid propellant rocket engines , Airframes , Pneumatic devices , Electrical equipment , Flight control systems , All inertial guidance , Guided missile tracking systems , Reentry vehicles , Propellant control , Atlas , Ma-3 propulsion systems , Xsm-65e missiles