Equations obtained for calculating divergence speed of multistage rocket; analysis assumes that total lift separates into components working on several points of rocket body and that inertial force of body is equated with separated lifts; aerodynamic characteristics values necessary to calculate divergence speed can be obtained by wind tunnel test of model and simple bending test of body.
Body divergence of multi-stage rocket
Tokyo. Univ -- Inst Space Aeronautical Science -- Report
1967
9 pages
Report
English
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Body Divergence of a Multi-Stage Rocket
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