Accession Number : AD0851567

Title :   Mercury Booster Working Group Flight Test Report Mercury/Atlas MA-3 (Atlas 100D) 25 April 1961.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date : 08 MAY 1961

Pagination or Media Count : 67

Abstract : The report describes the launch and flight parameters of an unmanned spacecraft.

Descriptors :   (*LAUNCH VEHICLES, FLIGHT TESTING), LAUNCHING SITES, GUIDED MISSILE TRAJECTORIES, ASCENT TRAJECTORIES, GUIDED MISSILE LAUNCHERS, GUIDED MISSILE COMPUTERS, AUTOMATIC PILOTS, FAILURE, GUIDED MISSILE SAFETY, PERFORMANCE(ENGINEERING), RELIABILITY(ELECTRONICS), DESTRUCTORS.

Subject Categories : Spacecraft Trajectories and Reentry
      Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE