Additively Manufactured Acrylonitrile-Butadiene-Styrene–Nitrous-Oxide Hybrid Rocket Motor with Electrostatic Igniter-Reference-Cited by-同舟云学术

Additively Manufactured Acrylonitrile-Butadiene-Styrene–Nitrous-Oxide Hybrid Rocket Motor with Electrostatic Igniter

Published:2015-07 Issue:4 Volume:31 Page:1217-1220
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Whitmore Stephen A.¹

Affiliation:

1. Mechanical and Aerospace Engineering Department, Utah State University, Logan, Utah 84322-4130

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35681

Reference10 articles.

1. Development of a Power Efficient, Restart-Capable Arc Ignitor for Hybrid Rockets

2. The thermal decomposition of nitrous oxide at pressures up to forty atmospheres

3. RhodesG. W. “Investigation of Decomposition Characteristics of Gaseous and Liquid Nitrous Oxide,” U.S. Air Force Weapons Lab., Rept. AD-784-602, Kirtland AFB, NM, July 1974.

4. BakerA. “Catalytic Decomposition of Nitrous Oxide, Final Report,” Surrey Satellite Technology Ltd. TR-SPDB-38569-03, England, UK, June 2003.

5. Catalytic Decomposition of Nitrous Oxide Monopropellant for Hybrid Motor Re-Ignition

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