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SMART- Small Motor AerRospace Technology

Author(s)
Viola, Franco  
Viola, Franco  
Balucani, M.
Crescenzi, R.
Ferrari, A.
Date Issued
2004-01-01
Abstract
This paper presents the SMART (Small Motor AerRospace Tecnology) propulsion system, constituted of microthrusters array realised by semiconductor technology on silicon wafers. SMART system is obtained gluing three main modules: combustion chambers, igniters and nozzles. The module was then filled with propellant and closed by gluing a piece of silicon wafer in the back side of the combustion chambers. The complete assembled module composed of 25 micro- thrusters with a 3 x 5 nozzle is presented. The measurement showed a thrust of 129 mN and impulse of 56,8 mNs burning about 70mg of propellant for the micro-thruster with nozzle and a thrust of 21 mN and impulse of 8,4 mNs for the micro-thruster without nozzle.
URI
https://hdl.handle.net/20.500.13025/1450
URL
http://adsabs.harvard.edu/abs/2004ESASP.571E..48B
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