Effect of Nitrocellulose Gasifying Binder on Thrust Performance and High‐g Launch Tolerance of Miniaturized Nanothermite Thrusters-Reference-Cited by-同舟云学术

Effect of Nitrocellulose Gasifying Binder on Thrust Performance and High‐g Launch Tolerance of Miniaturized Nanothermite Thrusters

Published:2014-04-30 Issue:3 Volume:39 Page:374-382
ISSN:0721-3115
Container-title:Propellants, Explosives, Pyrotechnics
language:en
Short-container-title:Propellants, Explosives, Pyrotechnics

Author:

Staley Clay S.¹²,Raymond Kristofer E.²,Thiruvengadathan Rajagopalan¹²,Herbst Jackson J.¹,Swaszek Sean M.³,Taylor Robert J.⁴,Gangopadhyay Keshab¹²,Gangopadhyay Shubhra¹

Affiliation:

1. Department of Electrical and Computer Engineering, University of Missouri, Columbia, MO 65211, USA

2. NEMS/MEMS Works, LLC. Columbia, MO 65211, USA

3. U.S. Army Armament Research, Development and Engineering Center, Picatinny Arsenal, NJ, 07806, USA

4. General Atomics, San Diego, CA, 92127, USA

Funder

U.S. Army Armament Research, Development and Engineering Center

Office of Naval Research

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.201400011

Reference56 articles.

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4. Design, fabrication and modeling of solid propellant microrocket-application to micropropulsion

5. Solid Propellant Microthruster Design for Nanosatellite Applications

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