General formulation of equations of motion for rocket consisting of 2 units rotating relative to each other about aerodynamic axis of symmetry; effects of rotation, and variation in gravitational field of Earth, as well as mass unbalance of rocket are taken into account.
Ballistic equations for seven degree of freedom rocket
Illinois Univ -- Dept Theoretical Applied Mechanics -- T A M Report
1961
77 pages
Report
Englisch
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