The primary purposes of the flight were to obtain data for statistical determination of CEP at the 6000 nautical mile range and to evaluate the ability of the mobile automatic programmed checkout equipment system and procedures to check out a missile in the missile assembly building. Detailed objectives are listed on the following page along with applicable comments relative to the degree of satisfaction. (Author)
WS 107A-1Flight Test Working Group Flight Test Report Atlas Missile 36E, 19 December 1961, AMR Range Test Number 5464 Astronautics Test Number P3-501-00-36
1961
88 pages
Report
No indication
English
Missile Technology , Surface to surface missiles , Flight testing , Circular error probable , Checkout equipment , Ground support equipment , Reentry vehicles , Miss distance , Airframes , Liquid propellant rocket engines , Propellant control , Pneumatic devices , Hydraulic equipment , Telemeter systems , Beacons , Transponders , Flight control systems , Inertial guidance , Guided missile tracking systems , Atlas , Azusa , Mark-5 reentry vehicles , Xsm-65e missiles