Electrospray Thruster for CubeSat-Reference-Cited by-同舟云学术

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Electrospray Thruster for CubeSat

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Ober Scott¹,Branam Richard¹,Huffman Richard¹,Demmons Nathaniel²,Martin Roy³

Affiliation:

1. Air Force Institute of Technology

2. Busek Company, Inc.

3. Busek Co. Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-522

Reference4 articles.

1. 1BusekCoInc.1UColloidThruster&ElectronicsOperationManual[Manual].Natick,MA,Nov.10,2010.

2. Microthruster Propulsion for the Space Technology 7 (ST7) Technology Demonstration Mission

3. 3Selstrom, J. Thrust and Performance Study of Micro Pulsed Plasma Thruster. MS Thesis, AFIT/GAE/ENY/10-M21. Graduate School of Engineering and Management,Air Force Institute of Technology (AU), Wright-Patterson AFB OH,March 2010.

4. 4Humble,R.Henry,G.andLarson,W. SpacePropulsionAnalysisandDesign,NewYork,NY:McGraw-Hill,1995.

Cited by 3 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. A STUDY ON THE RECENT ADVANCES IN THE DESIGN OF MEMS-BASED SOLID MICROTHRUSTERS;International Journal of Energetic Materials and Chemical Propulsion;2023

2. Microfabricated Electrospray Thruster Array with High Hydraulic Resistance Channels;Journal of Propulsion and Power;2017-07

3. Mission Analysis for CubeSats with Micropropulsion;Journal of Spacecraft and Rockets;2016-09

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