Approximate analytical solution for satellite orbits subjected to small thrust or drag.
- 1 June 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (6) , 1121-1128
- https://doi.org/10.2514/3.4147
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- On Take‐off from Circular Orbit by Small ThrustZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1964
- LOW CONSTANT TANGENTIAL THRUST SPIRAL TRAJECTORIESAIAA Journal, 1963
- Satellite Lifetimes in Elliptic OrbitsJournal of the Aerospace Sciences, 1962
- Survey of Current Literature on Satellite LifetimesARS Journal, 1962
- Theoretical evaluation of atmospheric drag effects in the motion of an artificial satelliteThe Astronomical Journal, 1961
- Air drag effect on a satellite orbit described by difference equations in the revolution numberQuarterly of Applied Mathematics, 1958