Test of B/Ti multilayer reactive igniters for a micro solid rocket array thruster-Reference-Cited by-同舟云学术

Test of B/Ti multilayer reactive igniters for a micro solid rocket array thruster

Published:2008-06 Issue:2 Volume:144 Page:361-366
ISSN:0924-4247
Container-title:Sensors and Actuators A: Physical
language:en
Short-container-title:Sensors and Actuators A: Physical

Author:

Tanaka Shuji,Kondo Kazuyuki,Habu Hiroto,Itoh Akihito,Watanabe Masashi,Hori Keiichi,Esashi Masayoshi

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Metals and Alloys,Surfaces, Coatings and Films,Condensed Matter Physics,Instrumentation,Electronic, Optical and Magnetic Materials

Reference10 articles.

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3. High-impulse, low-power, digital microthrusters using low boiling temperature liquid propellant with high viscosity fluid plug;Kang;Sens. Actuators A,2002

4. High-pressure bipropellant microrocket engine;London;J. Propul. Power,2001

5. MEMS-based solid propellant rocket array thruster with electrical feedthroughs;Tanaka;Trans. Jpn. Soc. Aeronaut. Space Sci.,2003

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