Recommended Practice for Thrust Measurement in Electric Propulsion Testing-Reference-Cited by-同舟云学术

Recommended Practice for Thrust Measurement in Electric Propulsion Testing

Published:2017-05 Issue:3 Volume:33 Page:539-555
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Polk James E.¹,Pancotti Anthony²,Haag Thomas³,King Scott⁴,Walker Mitchell⁴,Blakely Joseph⁵,Ziemer John¹

Affiliation:

1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

2. MSNW, LLC, Redmond, Washington 98052

3. NASA John H. Glenn Research Center, Cleveland, Ohio 44135

4. Georgia Institute of Technology, Atlanta, Georgia 30332

5. ERC, Inc., Edwards Air Force Base, California 93523

Funder

National Aeronautics and Space Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B35564

Reference47 articles.

1. Dynamic Response of Linear Mechanical Systems

2. Development of thrust stand for low impulse measurement from microthrusters

3. LakeJ.CavallaroG.SpanjersG.AdkisonP.DulliganM. “Resonant Operation of a Micro-Newton Thrust Stand,” U.S. Air Force Research Lab., Space and Missile Propulsion Division, TR AFRL-PR-ED-TP-2002-308, Edwards AFB, CA, 2003.

4. ST7-DRS Colloid Thruster System Development and Performance Summary

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