Thrust modulation of solid propellant rockets by a fluidic vortex valve with secondary combustion-Reference-Cited by-同舟云学术

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Thrust modulation of solid propellant rockets by a fluidic vortex valve with secondary combustion

Published:1982-12 Issue:12 Volume:9 Page:703-711
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Natan B.,Gany A.,Wolff H.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference4 articles.

1. A solid-propellant rocket motor modulated by a fluidic vortex valve;Walsh;J. Spacecraft,1971

2. Thrust modulation of solid propellant rockets by use of a fluidic vortex valve;Birk,1977

3. A computer program for complex chemical compositions incident and reflected shocks and Chapman-Jouguet detonations;Gordon;NASA SP-273,1971

4. Transonic swirling flow;Lewellen;AIAA J.,1969

Cited by 8 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 study of the effect of electric fields on the combustion characteristics of PMMA under lateral inflow;Acta Astronautica;2020-02

2. Study of the effect of DC high-voltage electric fields on the regression rate of PMMA;Acta Astronautica;2019-12

3. Swirl Characteristics of Vortex Valve Variable-Thrust Solid Rocket Motor;J APPL FLUID MECH;2018

4. Influence of Structural Parameters on the Performance of Vortex Valve Variable-Thrust Solid Rocket Motor;International Journal of Turbo & Jet-Engines;2017-01-01

5. Development of a Low-Cost Vortex-Cooled Thrust Chamber Using Hybrid Fabrication Techniques;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

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