Design and testing of a microelectromechanical-system-based high heat flux vaporizing liquid microthruster-Reference-Cited by-同舟云学术

Design and testing of a microelectromechanical-system-based high heat flux vaporizing liquid microthruster

Published:2020-05 Issue: Volume:170 Page:719-734
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Kwan Pok-Wang^ORCID,Huang Xun^ORCID,Zhang Xin^ORCID

Funder

Hong Kong University of Science and Technology

National Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference70 articles.

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4. The hybrid (hydrazine) resistojet, AIAA 5th Propulsion Joint Specialist Conference;Schreib;AIAA paper,1969

5. Design of high-performance resistojets for advanced spacecraft;Page,1971

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