Method for On-Orbit Thrust Estimation for Microthrusters Based on Nanosatellites-Reference-Cited by-同舟云学术

Method for On-Orbit Thrust Estimation for Microthrusters Based on Nanosatellites

Published:2022-03 Issue:2 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yang Qinglin¹,Zhou Weijing²^ORCID,Ye Jifei³,Chang Hao⁴^ORCID

Affiliation:

1. State Key Laboratory of Laser Propulsion and Application, Dept. of Aerospace and Technology, Space Engineering Univ., Beijing 101416, China.

2. Associate Professor, State Key Laboratory of Laser Propulsion and Application, Dept. of Aerospace and Technology, Space Engineering Univ., Beijing 101416, China (corresponding author). ORCID: .;

3. Associate Professor, State Key Laboratory of Laser Propulsion and Application, Dept. of Aerospace and Technology, Space Engineering Univ., Beijing 101416, China.

4. Assistant Professor, State Key Laboratory of Laser Propulsion and Application, Dept. of Aerospace and Technology, Space Engineering Univ., Beijing 101416, China. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001370

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5. Emhoff J. W. D. H. Simon and H. B. Land. 2016. “Development status of the micro thrust measurement technology based on cantilever beam structure.” In Proc. 11th Int. Conf. on Reliability Maintainability and Safety (ICRMS). New York: IEEE.