First order objectives of the flight included obtaining data on the re-entry vehicle impact location for the statistical determination of CEP, the evaluation of the flight control system performance, the evaluation of the inertial guidance system performance and accuracy and the evaluation of the performance of the acoustica PU system. (Author)
WS 107A-1Flight Test Working Group Flight Test Report Atlas Missile 25E 2 October 1961 AMR Range Test Number 1252, Astronautics Test Number P1-503-00-25
1961
88 pages
Report
Keine Angabe
Englisch
Missile Technology , Surface to surface missiles , Flight testing , Reentry vehicles , Impact prediction , Flight control systems , Inertial guidance , Propellant control , Miss distance , Telemeter systems , Pneumatic devices , Hydraulic equipment , Liquid propellant rocket engines , Guided missile tracking systems , Guided missile safety , Circular error probable , Atlas , Azusa , Xsm-65e missiles