Conference Proceeding
Refine
Year of publication
Institute
- Fachbereich Luft- und Raumfahrttechnik (198) (remove)
Has Fulltext
- no (198) (remove)
Document Type
- Conference Proceeding (198) (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)
- combustor development (2)
- fuels (2)
- industrial gas turbine (2)
- multiple NEA rendezvous (2)
- small spacecraft (2)
- Aircraft design (1)
- Antarctica (1)
- Asteroid Deflection (1)
- Attitude dynamics (1)
- Automated Optimization (1)
- Bumblebees (1)
- Capacity Building Higher Education (1)
- Correlations (1)
- Design rules (1)
- Drag (1)
- ESATAN (1)
- Electrical Flight (1)
- Emissions (1)
- Erasmus+ United (1)
- European Framework and South East Asia (1)
- Evolutionary Neurocontrol (1)
- Flame residence time (1)
- Flame temperature (1)
- Flight Mechanics (1)
- Flight Tests (1)
- Flight control (1)
- Fuel-flexibility (1)
- GEO (1)
- Gas turbine combustion (1)
- Geometry (1)
- Gossamer (1)
- Gossamer structures (1)
- Green aircraft (1)
- Guide Tube (1)
- Hybrid Propellants (1)
- Hybrid-electric aircraft (1)
- ITS (1)
- Inflight Regeneration, Recuperation (1)
- Infused Thermal Solutions (1)
- Interplanetary flight (1)
- Jupiter (1)
- Kalman filter (1)
- LEO (1)
- Low-Thrust Propulsion (1)
- MAV (1)
- Malaysian Automotive Industry (1)
- Malaysian automotive industry (1)
- Mars (1)
- Multiphase (1)
- NOx (1)
- Nozzle (1)
- Obstacle avoidance (1)
- Orbital dynamics (1)
- PEM fuel cells (1)
- PHILAE (1)
- Planetary Protection (1)
- Planetary exploration (1)
- Propeller Aerodynamics (1)
- Reusable Rocket Engines (1)
- Sequence-Search (1)
- Small Solar System Body Lander (1)
- Small Spacecraft (1)
- Solar Power Sail (1)
- Solar Sail (1)
- Solar sail (1)
- Spacecraft Trajectory Optimization (1)
- Statistics (1)
- Suction (1)
- TICTOP (1)
- Technology Transfer (1)
- UAV (1)
- UTeM Engineering Knowledge Transfer Unit (1)
- Unmanned Air Vehicle (1)
- aircraft engine (1)
- asteroid lander (1)
- asteroid sample return (1)
- avalanche (1)
- aviation application (1)
- combustion (1)
- combustor (1)
- control system (1)
- electrically driven compressors (1)
- electro mobility (1)
- emission (1)
- emission index (1)
- engine demonstration (1)
- flotilla missions (1)
- fuel cell (1)
- fuel cell systems (1)
- gas turbine (1)
- habitability (1)
- health management systems (1)
- heliosphere (1)
- ice moons (1)
- icy moons (1)
- internal combustion engine (1)
- ion propulsion (1)
- latent heat (1)
- lattice (1)
- life detection (1)
- low-thrust (1)
- low-thrust trajectory optimization (1)
- near-Earth asteroid (1)
- nitric oxides (1)
- passive thermal control (1)
- planetary defence (1)
- responsive space (1)
- sample return (1)
- small solar system body characterisation (1)
- small spacecraft asteroid lander (1)
- small spacecraft solar sail (1)
- snow (1)
- solar sails (1)
- solar system (1)
- space missions (1)
- star tracker (1)
- subroutine (1)
- system engineering (1)
- technology transfer (1)
- thermo-physical (1)
- underwater vehicle (1)
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.