Spacecraft guidance in the Martian atmosphere
Abstract
The handbook discusses spacecraft guidance in the Martian atmosphere during descent and reentry into satellite orbit. Mars is considered with reference to its atmosphere, winds, and cloud cover and their effect on spacecraft guidance. Procedures for effecting a soft landing are proposed, noting rocket engine configurations, parachute systems, and ballistics. Orbital-descent characteristics are outlined, including aerodynamic deceleration and control algorithms.
- Publication:
-
Moscow Izdatel Nauka
- Pub Date:
- 1977
- Bibcode:
- 1977MoIzN....Q....I
- Keywords:
-
- Atmospheric Entry;
- Mars Atmosphere;
- Mars Probes;
- Spacecraft Guidance;
- Aerodynamic Drag;
- Algorithms;
- Ballistics;
- Deceleration;
- Descent Trajectories;
- Mars Landing;
- Optimal Control;
- Orbit Calculation;
- Parachute Descent;
- Soft Landing;
- Spacecraft Configurations;
- Trajectory Optimization;
- Astrodynamics