Stability of a Dual-Spin Satellite in Circular Orbit
Journal of Spacecraft and Rockets1971Vol. 8(10), pp. 1092–1094
Abstract
Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.
Related Papers
- → Orbital re-entry experiment vehicle ground and flight dynamic test results comparison(1996)19 cited
- → Launch Vehicle Atmospheric Flight Loads(2000)2 cited
- → Space vehicle glow and its impact on spacecraft systems(1988)43 cited
- → Optimal payload trajectory characteristics for horizontally launchedbooster vehicle.(1968)2 cited
- → Power systems for an unmanned lunar roving vehicle.(1966)