Design and test planning for a 250-klbf-thrust hybrid rocket motor under the Hybrid Propulsion Demonstration Program-Reference-Cited by-同舟云学术

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Design and test planning for a 250-klbf-thrust hybrid rocket motor under the Hybrid Propulsion Demonstration Program

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Boardman T.¹,Abel T.²,Claflin S.³,Shaeffer C.⁴,Boardman T.¹,Abel T.²,Claflin S.³,Shaeffer C.⁴

Affiliation:

1. Thiokol Corp., Brigham City, UT

2. Lockheed Martin Astronautics, Huntsville, AL

3. Boeing North American/Rocketdyne Div., Canoga Park, CA

4. Pratt & Whitney, Chemical Systems Div., San Jose, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2804

Reference4 articles.

1. Hybrid propulsion for launch vehicle boosters - A program status update

Cited by 11 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. A Review of Recent Developments in Hybrid Rocket Propulsion and Its Applications;Aerospace;2024-09-09

2. Bridging the Technology Gap: Strategies for Hybrid Rocket Engines;Aerospace;2023-10-22

3. Effect of Protrusion Configuration on Combustion Stability of Hybrid Rocket Motor;Proceedings of the National Aerospace Propulsion Conference;2022-07-24

4. Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy;Acta Astronautica;2021-11

5. Experimental Studies of Protrusion-Inserted Hybrid Rocket Motor with Varying L/D Ratio;Journal of Spacecraft and Rockets;2021-01

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