Low temperature co-fired ceramic vaporizing liquid microthruster for microspacecraft applications-Reference-Cited by-同舟云学术

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Low temperature co-fired ceramic vaporizing liquid microthruster for microspacecraft applications

Published:2012-09 Issue: Volume:97 Page:577-583
ISSN:0306-2619
Container-title:Applied Energy
language:en
Short-container-title:Applied Energy

Author:

Karthikeyan K.,Chou S.K.,Khoong L.E.,Tan Y.M.,Lu C.W.,Yang W.M.

Publisher

Elsevier BV

Subject

Management, Monitoring, Policy and Law,Mechanical Engineering,General Energy,Building and Construction

Reference20 articles.

1. Mueller J. Thruster options for microspacecraft: a review and evaluation of existing hardware and emerging technologies. In: 33rd AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit AIAA 3058; 1997.

2. Bayt RL. Analysis, fabrication, and testing of a MEMS-based micropropulsion system. PhD dissertation, Massachusetts Institute of Technology; 1999.

3. Development of a low-temperature co-fired ceramic solid propellant microthruster;Zhang;J Micromech Microeng,2005

4. Development of a solid propellant microthruster with chamber and nozzle etched on a wafer surface;Zhang;J Micromech Microeng,2004

5. Design, fabrication and modeling of solid propellant microrocket-application to micropropulsion;Rossi;Sensor Actuat,2002

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