Accession Number : AD0606091

Title :   OPTIMUM PROGRAM FOR SINGLE STAGE ROCKETS IN WHICH EXPELLANT IS NOT THE SOURCE OF POWER,

Corporate Author : THOMPSON RAMO WOOLDRIDGE INC LOS ANGELES CALIF

Personal Author(s) : Irving,J. H.

Report Date : 07 OCT 1956

Pagination or Media Count : 17

Abstract : The gravitational force and the thrust force are considered in the derivation of an optimum mass rate and exhaust velocity program.

Descriptors :   (*ROCKET TRAJECTORIES, OPTIMIZATION), ROCKETS, GRAVITY, THRUST, ROCKET PROPULSION, EQUATIONS, MOTION

Distribution Statement : APPROVED FOR PUBLIC RELEASE