Blowdown pulser design criteria for solid-propellant rockets-Reference-Cited by-同舟云学术

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Blowdown pulser design criteria for solid-propellant rockets

Published:1986-03 Issue:2 Volume:2 Page:110-116
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Brown R. S.¹

Affiliation:

1. United Technologies Chemical Systems Division, San Jose, California

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/10.2514/3.22853

Reference15 articles.

1. Pulsing techniques for solid-propellant rocket motors - Modeling andcold-flow testing

2. Pulse-Triggered Instability in Solid Rocket Motors

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. Pulsed Instability Investigation of a Dual Thrust Solid Propellant Motor;AIAA Propulsion and Energy 2020 Forum;2020-08-17

2. Experimental and theoretical study on characteristics of pulse excitation in T-burners;Acta Astronautica;2017-05

3. Vorticity and Turbulence Effects on Combustion Stability of Solid Propellant Rocket Motors;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

4. Nonlinear Stability Testing of Full-Scale Tactical Motors;Journal of Propulsion and Power;1997-05

5. Applications of Combustion-Stability Technology to Solid-Propellant Rocket Motors;Nonsteady Burning and Combustion Stability of Solid Propellants;1992-01-01

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