Closed-Loop Thrust and Pressure Profile Throttling of a Nitrous-Oxide HTPB Hybrid Rocket Motor-Reference-Cited by-同舟云学术

Closed-Loop Thrust and Pressure Profile Throttling of a Nitrous-Oxide HTPB Hybrid Rocket Motor

Published:2012-07-30 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
language:
Short-container-title:

Author:

Peterson Zachary,Eilers Shannon,Whitmore Stephen

Publisher

American Institute of Aeronautics and Astronautics

Reference52 articles.

1. 2Safie, F. M. and Fox, E. P. “A Probabilistic Design Analysis Approach for Launch Systems,” 27th AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference, Vol. AIAA-1991-3372, 1991.

2. 3Maggie, G. “Space Shuttle Probabilistic Risk Assessment: Methodology and Application,” International Symposium on Product Quality and Integrity, Proceedings of the Reliability and Maintainability Symposium, Las Vegas NV, 1996.

Cited by 6 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. Numerical Simulation of Chemical Propulsion Systems: Survey and Fundamental Mathematical Modeling Approach;Aerospace;2023-09-26

2. Model Reference Adaptive Control of a Ball Valve for Hybrid Rocket Throttling Application;2023 9th International Conference on Control, Decision and Information Technologies (CoDIT);2023-07-03

3. Ballistic Characterization of Armored Grains with Vortex Flow Pancake Hybrid Rocket Engine;AIAA SCITECH 2023 Forum;2023-01-19

4. Closed Loop Throttle Control of a Liquefying Fuel Hybrid Rocket Motor;Journal of Aerospace Technology and Management;2021

5. Deep Throttle of a Nitrous Oxide and Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor;Journal of Propulsion and Power;2014-01