Ballistic Properties of Mixed Hybrid Propellants-Reference-Cited by-同舟云学术

Ballistic Properties of Mixed Hybrid Propellants

Published:2004-06-21 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Frederick Robert¹,Moser Marlow¹,Knox Richard²,Whitehead Joshua¹

Affiliation:

1. UAH Propulsion Research Center

2. University of Alabama in Huntsville

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3824

Reference8 articles.

1. 1"A Short Course on Concepts, Systems, Applications, and Operating Principles of Hybrid Rockets," AIAA Hybrid RocketTechnical Committee,Washington,D.C., July1995.

2. 3Wampler, J., etal "Conceptual Design of Hybrid Rocket Powered Upper Stage (HRPUS) Demonstrator," Design Report,TheUniversityofAlabamainHuntsville,Huntsville,AL.,1996.

3. 4Cornell,J.A.,ExperimentswithMixtures,2nded.,JohnWiley&Sons,Inc.,1990.

4. Regression Rate Behavior of Hybrid Rocket Solid Fuels

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Ramjet Fuel Mixture Optimization;AIAA Propulsion and Energy 2020 Forum;2020-08-17

2. Thermal Analysis Techniques and Autoignition Testing for Solid Polymers: a Review;AIAA Propulsion and Energy 2019 Forum;2019-08-16

3. Burning Rate Optimization Under Uncertainty Using Response Surfaces and Monte Carlo Simulation;Journal of Propulsion and Power;2014-07

4. Study on Thermal Degradation Characteristics of Pre-Treated Paraffin;Applied Mechanics and Materials;2014-01

5. The experiments for the enhancement of regression rate of hybrid rocket fuel;Journal of Mechanical Science and Technology;2005-10