Ascent or Descent from Satellite Orbit by Low Thrust
- 1 December 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (12) , 2203-2209
- https://doi.org/10.2514/3.55302
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Satellite motion for arbitrary eccentricity and inclination around the smaller primary in the restricted three-body problemThe Astronomical Journal, 1966
- Optimum guidance for a low thrust interplanetary vehicle.AIAA Journal, 1966
- Take-Off from a Circular Orbit by a Small ThrustPublished by Elsevier ,1966
- Comparison of the Modified Method of Averaging and the Two Variable Expansion ProcedureSIAM Review, 1966
- Low-thrust spiral trajectory of a satellite of variable mass.AIAA Journal, 1965
- Perturbation solutions for low-thrust rocket trajectories.AIAA Journal, 1965
- A natural first approximation to low-thrust trajectories between satellite orbits of the earth and moonAIAA Journal, 1965
- 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
- Uniformly Valid Asymptotic Approximations for Certain Non-Linear Differential EquationsPublished by Elsevier ,1963