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.

1. Experimental propulsion performance of a low power pulsed resistojet, 2nd Aerospace Sciences Meeting;Bennet;AIAA paper,1965

2. 3-kW concentric tubular resistojet performance;Page;J. Spacecr. Rocket.,1966

3. Definition of a Resistojet Control System for the Manned Orbital Research Laboratory. Volume 5 - Resistojet Design and Development Final Report, Tech. rep., NASA, USA;Page,1968

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

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Towards an optimized heat transfer process in vaporizing liquid microthrusters using pulsed heating control;Acta Astronautica;2024-06

2. Comparative analytical analysis and component selection of resistojet thruster for satellite propulsion;Journal of Space Safety Engineering;2024-03

3. Additively manufactured vaporizing liquid microthruster with micro pin fins for enhanced heat transfer;Acta Astronautica;2022-10

4. MEMS Vaporazing Liquid Microthruster: A Comprehensive Review;Applied Sciences;2021-09-26

5. Flow regime characterization of a silicon-based vaporizing liquid microthruster;Acta Astronautica;2021-08