Approximation method for orbital transfer propulsion system requirements in central force field
An approximation method for determination of propulsion requirements associated with low thrust coplanar orbital transfer in a central force field under negligible external perturbations
1963-01-01
Miscellaneous
No indication
English
Thrust Limited Coplanar Aeroassisted Orbital Transfer
AIAA | 2001
|FULL-LENGTH PAPERS - Thrust Limited Coplanar Aeroassisted Orbital Transfer
Online Contents | 2001
|Orbit Raising and De-Orbit for Coplanar Satellite Constellations with Low-Thrust Propulsion
BASE | 2018
|