Comment on "Dynamic Analysis for Lunar Alightment"
- 1 September 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (9) , 2196-2197
- https://doi.org/10.2514/3.54973
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- NONEQUATORIAL LAUNCHING TO EQUATORIAL ORBITS AND GENERAL NONPLANAR LAUNCHINGAIAA Journal, 1963
- DYNAMIC ANALYSIS FOR LUNAR ALIGHTMENTAIAA Journal, 1963
- A NOTE ON THE CLASSICAL BUCKLING LOAD OF CIRCULAR CYLINDRICAL SHELLS UNDER AXIAL COMPRESSIONAIAA Journal, 1963
- The perturbed motion of 24-hour satellites due to equatorial ellipticityJournal of Geophysical Research, 1963
- Perturbations of a Synchronous Satellite Due to Triaxiality of the EarthJournal of the Aerospace Sciences, 1962
- Effect of ellipticity of the equator on 24-hour nearly circular satellite orbitsJournal of Geophysical Research, 1962
- Optimum Maneuvers for Launching Satellites Into Circular Orbits of Arbitrary Radius and InclinationARS Journal, 1961