Sizing of Solar Thermal Thruster for Satellite Orbital Control Using High Thrust One Tangent Burn
19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
2014-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2014
|Constant-Thrust Orbital Transfer About Binary Asteroids Using Bilinear Tangent Guidance
IEEE | 2024
|Thrust of Solar Thermal Thruster Under Variable Working Conditions
Springer Verlag | 2024
|Optimum burn scheduling for low-thrust orbital transfers
AIAA | 1989
|