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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite