Numerical analysis of a miniaturised cold gas thruster for micro‐ and nano‐satellites-Reference-Cited by-同舟云学术

Numerical analysis of a miniaturised cold gas thruster for micro‐ and nano‐satellites

Published:2011-03-08 Issue:2 Volume:28 Page:184-195
ISSN:0264-4401
Container-title:Engineering Computations
language:en
Short-container-title:Engineering Computations

Author:

Grm Aleksander,Grönland Tor‐Arne,Rodič Tomaž

Publisher

Emerald

Subject

Computational Theory and Mathematics,Computer Science Applications,General Engineering,Software

Reference2 articles.

1. Ketsdever, A. and Mueller, J. (1999), “Systems considerations and design options for microspacecraft propulsion systems”,AIAA Paper, Los Angeles, CA, p. 2723.

2. Mueller, J. (2000), “Thruster options for microspacecraft: a review and evaluation of the state‐of‐the art and emerging technologies”,Micropropulsion for Small Spacecraft AIAA Progress in Astronautics and Aeronautics, Reston, VA, Vol. 187, pp. 45‐137.

Cited by 4 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. 微牛级变推力控制技术和无拖曳卫星平台的噪声问题: 综述;Journal of Zhejiang University-SCIENCE A;2023-10

2. Evaluating the necessity of application of partial slip formulations to micro-nozzles operating under marginally rarefied flow regimes;2ND INTERNATIONAL CONFERENCE ON MATHEMATICAL TECHNIQUES AND APPLICATIONS: ICMTA2021;2022

3. Investigation of non-equilibrium boundary conditions considering sliding friction for micro/nano flows;International Journal of Numerical Methods for Heat & Fluid Flow;2019-08-05

4. Nanosatellite orbit control using MEMS cold gas thrusters;Proceedings of the Estonian Academy of Sciences;2014