Back to Search
Start Over
Study on the physicalmechanism of a plasma thruster with wide range of thrust
- Source :
- 2014 IEEE 41st International Conference on Plasma Sciences (ICOPS) held with 2014 IEEE International Conference on High-Power Particle Beams (BEAMS).
- Publication Year :
- 2014
- Publisher :
- IEEE, 2014.
-
Abstract
- Considerable progress has been made in recent years in the study of the Earth's gravitational field by observing the motion of satellites in low altitude orbits. However, such observations are hampered by the aerodynamic drag caused by the residual atmosphere, which modifies the orbits of these satellites in an unpredictable way. In order to overcome this problem, an on-board propulsion system with wide range of thrust is needed which will exactly balance the drag experienced by the spacecraft while measurements are being made.
- Subjects :
- Physics
Ion thruster
Spacecraft propulsion
business.industry
Thrust
Variable Specific Impulse Magnetoplasma Rocket
Classical mechanics
Drag
Physics::Space Physics
Field-emission electric propulsion
Aerodynamic drag
Astrophysics::Earth and Planetary Astrophysics
Pulsed inductive thruster
Aerospace engineering
business
Physics::Atmospheric and Oceanic Physics
Subjects
Details
- Database :
- OpenAIRE
- Journal :
- 2014 IEEE 41st International Conference on Plasma Sciences (ICOPS) held with 2014 IEEE International Conference on High-Power Particle Beams (BEAMS)
- Accession number :
- edsair.doi...........0a9100fc195b052f4f5b21a381ac2da4
- Full Text :
- https://doi.org/10.1109/plasma.2014.7012432