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Experimental and Numerical Investigation on Attitude Adjustment Characteristics of Spacecraft with Impulse Thruster

Published Online: 2024-09-09

Published Print: 2025-04

Authors

Su, Dongjian

Tao, Ruyi https://orcid.org/0009-0007-9390-7961
Wang, Hao

Jiang, Chunlei
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Text and Data Mining valid from 2024-09-09

Version of Record valid from 2024-09-09
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Article History

Received: 9 April 2024

Revised: 30 July 2024

Accepted: 27 August 2024

First Online: 9 September 2024

Declarations

:

: The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

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