Accession Number : AD0637670
Title : MAXIMUM PAYLOAD IN ORBIT.
Descriptive Note : Technical rept.
Corporate Author : LOCKHEED MISSILES AND SPACE CO SUNNYVALE CALIF
Personal Author(s) : Bryson,A. E.
Report Date : JUL 1961
Pagination or Media Count : 14
Abstract : An existing multistage rocket booster is considered along with a variable payload stage. For a given launch weight, the fuel allocation to each stage and the thrust-direction program are determined which will place the maximum payload into a specified orbit. (Author)
Descriptors : (*LAUNCH VEHICLES, *PAYLOAD), OPTIMIZATION, ORBITS, ASTRONAUTICS
Subject Categories : Spacecraft Trajectories and Reentry
Ground Support Sys & Facil For Space Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE