DocumentCode
447722
Title
Application of high power millimeter-wave to space propulsion
Author
Oda, Y. ; Ushio, M. ; Komurasaki, K. ; Takahashi, K. ; Kasugai, A. ; Sakamoto, K.
Author_Institution
Dept. of Adv. Energy, Tokyo Univ., Chiba, Japan
Volume
1
fYear
2005
fDate
19-23 Sept. 2005
Firstpage
30
Abstract
A microwave beaming thruster boosted by a 170GHz gyrotron was investigated. Plasma was successfully initiated by focusing the millimetre wave beam using a parabolic reflector. The plasma propagation velocity was increased with the beam power density; the velocity became supersonic at the power density beyond 80 kW/cm2. Propulsive impulse was measured through the flight experiments, and resulting momentum coupling coefficient, a ratio of thrust to input energy, was found drastically increased when the plasma propagation velocity becomes supersonic.
Keywords
aerospace propulsion; aerospace testing; gyrotrons; 170 GHz; beam power density; gyrotron; high power millimeter-wave; microwave beaming thruster; millimetre wave beam; momentum coupling coefficient; parabolic reflector; plasma propagation velocity; propulsive impulse; space propulsion; supersonic velocity; Energy measurement; Gyrotrons; Microwave propagation; Millimeter wave propagation; Particle beams; Plasma applications; Plasma density; Plasma measurements; Plasma waves; Propulsion;
fLanguage
English
Publisher
ieee
Conference_Titel
Infrared and Millimeter Waves and 13th International Conference on Terahertz Electronics, 2005. IRMMW-THz 2005. The Joint 30th International Conference on
Print_ISBN
0-7803-9348-1
Type
conf
DOI
10.1109/ICIMW.2005.1572391
Filename
1572391
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