Conference Proceeding
Refine
Year of publication
Institute
- Fachbereich Luft- und Raumfahrttechnik (197) (remove)
Has Fulltext
- no (197) (remove)
Document Type
- Conference Proceeding (197) (remove)
Keywords
- hydrogen (4)
- solar sail (4)
- MASCOT (3)
- GOSSAMER-1 (2)
- Hydrogen (2)
- Micromix (2)
- NOx emissions (2)
- PCM (2)
- Spacecraft (2)
- Trajectory Optimization (2)
Auslegung der CFK-Sandwich-Rumpfstruktur eines Hubschraubers mit der Methode der Finiten Elemente
(1994)
Solar sailcraft provide a wide range of opportunities for high-energy low-cost missions. To date, most mission studies require a rather demanding performance that will not be realized by solar sailcraft of the first generation.
However, even with solar sailcraft of moderate performance, scientifically relevant missions are feasible. This is demonstrated with a Near Earth Asteroid sample return mission and various planetary rendezvous missions.