
Accession Number : AD0675546
Title : ACCELERATION REQUIRED TO MANEUVER ONE SATELLITE AROUND ANOTHER AT CLOSE RANGE,
Corporate Author : RAND CORP SANTA MONICA CALIF
Personal Author(s) : Rowell,L. N.
Report Date : JUL 1968
Pagination or Media Count : 48
Abstract : Equations are derived for computing the components of acceleration required either to maintain two earth satellites in a fixed relative position or to move one satellite relative to another in a prescribed manner. These equations are applied to determine the total instantaneous acceleration required for several different fixed relative positions and motions of two satellites at close range. Then, for some cases, the required acceleration is related to the propulsive energy required by computing the ratio of propellant weight to initial weight for missions of up to 100day duration using specific impulses of 300, 1000, and 10,000 seconds. (Author)
Descriptors : (*MANEUVERING SATELLITES, *ASTRONAUTICS), EQUATIONS OF MOTION, CIRCULAR ORBITS, ELLIPTICAL ORBIT TRAJECTORIES, PERTURBATION THEORY, FUEL CONSUMPTION, ACCELERATION
Subject Categories : Astronautics
Spacecraft Trajectories and Reentry
Distribution Statement : APPROVED FOR PUBLIC RELEASE