A three-point propulsion system of an orbital deployment space module for at least one satellite including: chassis including exactly three first housings shaped to each receive a propulsion unit and at least one second housing shaped to receive a tank, at least one liquid fuel tank disposed in a second housing, and exactly three propulsion units, each propulsion unit being disposed in one of the first housings, and each propulsion unit including at least one thruster.
ORBITAL DEPLOYMENT MODULE WITH A THREE-POINT SPACE PROPULSION SYSTEM
2025-03-13
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
SLUB | 1984
SLUB | 1984
Reactionless orbital propulsion using tether deployment
NTRS | 1990
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