Publikationsdatum:
2019-08-14
Beschreibung:
The Propulsion System and Orbit Maneuver Integration in CubeSats project aims to solve the challenges of integrating a micro electric propulsion system on a CubeSat in order to perform orbital maneuvers and control attitude. This represents a fundamentally new capability for CubeSats, which typically do not contain propulsion systems and cannot maneuver far beyond their initial orbits.
Schlagwort(e):
Spacecraft Propulsion and Power; Astrodynamics
Materialart:
NASA FS-2015-03-30-ARC
,
ARC-E-DAA-TN25939
Format:
application/pdf