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Title:Ballistic equations for seven degree of freedom rocket
Author(s):Wilms, E.; Stippes, M.
Subject(s):Ballistics
Rockets
Abstract:This report contains a general formulation of the equations of motion for a rocket consisting of two units rotating relative to each other about an aerodynamic axis of symmetry. The effects of the rotation, and variation in the gravitational field of the earth, as well as the mass unbalance of the rocket are taken into account.
Issue Date:1961-11
Publisher:Department of Theoretical and Applied Mechanics. College of Engineering. University of Illinois at Urbana-Champaign
Series/Report:TAM R 204
1967-0500
Genre:Technical Report
Type:Text
Language:English
URI:http://hdl.handle.net/2142/111919
ISSN:0073-5264
Sponsor:Department of the Army, Redstone Arsenal, Project No. 5B99-01-004, DA-11-022-506-ORD-3488, ORD Project No. TW-205
Rights Information:Copyright 1961 Board of Trustees of the University of Illinois
Date Available in IDEALS:2021-11-04


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  • Technical Reports - Theoretical and Applied Mechanics (TAM)
    TAM technical reports include manuscripts intended for publication, theses judged to have general interest, notes prepared for short courses, symposia compiled from outstanding undergraduate projects, and reports prepared for research-sponsoring agencies.

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