Zhang, K. L. and Chou, S. K. and Ang, S. S. and Tang, X. S. (2005) A MEMS-based solid propellant microthruster with Au/Ti igniter. Sensors and Actuators A: Physical, 122 (1). 113 - 123.
Full text is not hosted in this archive but may be available via the Official URL, or by requesting a copy from the corresponding author.
Official URL: http://www.sciencedirect.com/science/article/B6THG...
A solid propellant microthruster with Au/Ti igniter is demonstrated as an improved micropropulsion system for microspacecraft. The new design provides the microthruster with a high degree of flexibility, maneuverability and integration. Single microthruster and microthruster arrays have been successfully fabricated using standard microfabrication technologies. The propellant combustion process in the micro-chamber of the microthruster has been visually observed. Initial tests employing gunpowder-based solid propellants, have produced 2.11 × 10−5 to 1.15 × 10−4 N s of total impulse and 2.68–14.65 s of specific impulse at sea level, and 3.52 × 10−5 to 2.22 × 10−4 N s of total impulse and 4.48–28.29 s of specific impulse in vacuum. The performance of the solid propellant microthruster with Au/Ti igniter is also compared with that of a solid propellant microthruster having a wire igniter.
|Additional Information:||SSSAMW 04 - Special Section of the Micromechanics Section of Sensors and Actuators based on contributions revised from the Technical Digest of the 2004 Solid-State Sensor, Actuator and Microsystems Workshop.|
|Uncontrolled Keywords:||MEMS; Micropropulsion; Microthruster; Solid propellant; Au/Ti igniter|
|Subjects:||Analytical Science > Nanotechnology for sensing and actuating|
Engineering > Nanotechnology applications in ICT
|Deposited On:||08 Apr 2009 17:34|
|Last Modified:||08 Apr 2009 17:34|
Repository Staff Only: item control page