Accession Number : ADA335740
Title : Optimal Non-Coplanar Launch to Quick Rendezvous
Descriptive Note : Doctoral thesis
Corporate Author : AIR FORCE INST OF TECH WRIGHT-PATTERSONAFB OH
Personal Author(s) : Sears, Gregory B.
PDF Url : ADA335740
Report Date : DEC 1997
Pagination or Media Count : 79
Abstract : The purpose of this study was to determine the feasibility of launching a Delta Clipper-like vehicle on an optimal, non-coplanar trajectory to rendezvous with an earth orbiting object in one orbit or less. The focus of the research was to determine what such a trajectory would look like, and to determine the cost, in payload mass, of flying such a trajectory. A model for the ascent trajectory was developed using the dynamics equations of motion, an atmosphere model, and an aerodynamic model for the DC-Y concept vehicle. A boundary value problem was posed and solved for a coplanar rendezvous. The non-coplanar solutions were obtained through extrapolation from the coplanar solution.
Descriptors : *RENDEZVOUS TRAJECTORIES, ORBITS, PAYLOAD, EQUATIONS OF MOTION, EARTH ORBITS, DYNAMICS, COSTS, SOLUTIONS(GENERAL), FEASIBILITY STUDIES, BOUNDARY VALUE PROBLEMS, PLANAR STRUCTURES, LAUNCHING, ATMOSPHERE MODELS, AERODYNAMICS, ASCENT TRAJECTORIES.
Subject Categories : Spacecraft Trajectories and Reentry
Distribution Statement : APPROVED FOR PUBLIC RELEASE