Improved Design and Characterization of MicroNewton Torsional Balance Thrust Stand-Reference-Cited by-同舟云学术

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Improved Design and Characterization of MicroNewton Torsional Balance Thrust Stand

Published:2013-07-12 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
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Author:

Cofer Anthony G.¹,Heister Stephen D.¹,Alexeenko Alina¹

Affiliation:

1. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3856

Reference8 articles.

1. Thrust Stand Micromass Balance for the Direct Measurement of Specific Impulse

2. A. H.Yan, B. C. Appel, and G.G.Jacob."MilliNewtonThrustStand CalibrationUsing ElectrostaticFins." AIAApaper 2009-212.

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