Simulation of Deployment Dynamics of Spinning Spacecraft
1967
25 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Environment simulation , Spacecraft design , Spin stabilization , Test method , Analog , Analysis , Appendage , Centrifugal , Computer , Conservation , Coriolis effect , Deployment , Design , Digital , Dynamics , Effect , Energy , Environment , Facility , Formulation , Gravity , Inertia , Kinematics , Kinetic , Method , Momentum , Numerical , Simulation , Solution , Spacecraft , Spin , Stabilization , Test
Simulation of deployment dynamics of spinning spacecraft
NTRS | 1967
|Simulation of deployment dynamics of spinning spacecraft
TIBKAT | 1967
|Simulation of deployment dynamics of spinning spacecraft
AIAA | 1967
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AIAA | 1963
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