
Accession Number : AD0860125
Title : Optimum Fuel Consumption Trajectory For SingleStage Missile.
Descriptive Note : Master's thesis,
Corporate Author : AIR FORCE INST OF TECH WRIGHTPATTERSON AFB OH SCHOOL OF ENGINEERING
Personal Author(s) : Pyle, Jerry W. ; Foote, Austin L.
Report Date : JUN 1969
Pagination or Media Count : 109
Abstract : The thesis presents the basic computer algorithm to obtain an optimal thrust profile for the launch of a onestage rocket boosted missile. The basic equations include the effects of: a round earth, the earth's rotation, and the atmosphere (drag). A complete derivation of the equations and an explanation of the computer algorithm are given. Appendix 8 contains a copy of the computer program. The result of applying the algorithm to a booster configuration is given as an example. (Author)
Descriptors : (*SURFACE TO SURFACE MISSILES, MATHEMATICAL MODELS), (*ROCKET ENGINES, THRUST), (*FUEL CONSUMPTION, OPTIMIZATION), COMPUTER PROGRAMMING, ALGORITHMS, THESES, MATHEMATICAL MODELS, COMPUTER PROGRAMS.
Subject Categories : Computer Programming and Software
Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE