평판형 MEMS 고체 추진제 추력기 요소 제작 및 성능 평가Fabrication, Performance Evaluation of Components of Planar Type MEMS Solid Propellant Thruster

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The MEMS solid propellant thrusters have very low thrust level for applying to the propulsion system of micro/nano satellites or the side jet thruster of smart bombs. In this research, the fabrication possibility of planar type MEMS solid propellant thrusters that have enlarged burning surface area was examined and the safety of the structure of thruster during the firing test was confirmed. The performance of a micro igniter which is the key component of the MEMS solid propellant thruster was estimated by the ANSYS Icepak and evaluated by the experiment. Finally, the thrust was measured by the micro force sensor. The levels of thrust were 300, 600 mN in the case of K=15, 20.
Publisher
한국항공우주학회
Issue Date
2008-06
Language
Korean
Citation

한국항공우주학회지, v.36, no.6, pp.581 - 586

ISSN
1225-1348
URI
http://hdl.handle.net/10203/87486
Appears in Collection
AE-Journal Papers(저널논문)
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