The purposes of the flight were to obtain data for statistical determination of CEP, evaluate the PU System, investigate the boattail heating and staging problems, evaluate the inertial guidance system performance, the re-entry vehicle performance and the performance of the arming and fuzing system. (Author)
WS 107A-1Flight Test Working Group. Flight Test Report, Atlas Missile 8F
1962
107 pages
Report
Keine Angabe
Englisch
Missile Technology , Surface to surface missiles , Flight testing , Circular error probable , Statistical analysis , Propellant control , Inertial guidance , Reentry vehicles , Guided missile warheads , Guided missile fuzes , Telemeter systems , Atmosphere entry , Miss distance , Atlas , Xsm-65f missiles