Design and testing of miniaturized plasma sensor for measuring hypervelocity impact plasmas-Reference-Cited by-同舟云学术

Design and testing of miniaturized plasma sensor for measuring hypervelocity impact plasmas

Published:2015-04 Issue:4 Volume:86 Page:043304
ISSN:0034-6748
Container-title:Review of Scientific Instruments
language:en
Short-container-title:Review of Scientific Instruments

Author:

Goel A.¹,Tarantino P. M.¹,Lauben D. S.¹,Close S.¹

Affiliation:

1. Department of Aeronautics and Astronautics, Stanford University, Stanford, California 94305, USA

Funder

National Aeronautics and Space Administration (NASA)

Publisher

AIP Publishing

Subject

Instrumentation

Link

http://aip.scitation.org/doi/pdf/10.1063/1.4917276

Reference33 articles.

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3. The proliferation of orbiting fragments: A simple mathematical model

4. Electromagnetic pulses generated by meteoroid impacts on spacecraft

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