Pressure oscillations in post-Challenger Space Shuttle redesigned solid rocket motors (RSRMs)
Author:
Affiliation:
1. U.S. Navy, Naval Weapons Center, China Lake, CA
2. Comarco, Inc., Ridgecrest, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-203
Reference8 articles.
Cited by 4 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. Investigation of Acoustic Instability in Solid-Propellant Rocket Motors with the Use of a Pulsed T-Burner;Combustion, Explosion, and Shock Waves;2021-07
2. Lessons Learned In Solid Rocket Combustion Instability;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08
3. Thrust Oscillations in Reduced Scale Solid Rocket Motors Part I : Experimental Investigations;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10
4. Comparison between firing tests and numerical simulation of vortex shedding in a 2-D test solid motor;23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference;1993-07-06
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