Solid Rocket Motor Design for a High Altitude Composite Rocket

2009 ◽  
Author(s):  
Eric Joyce ◽  
Michael Snyder
Keyword(s):  
High Altitude ◽  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Motor Design ◽  
Solid Rocket

Rapid Solid Rocket Motor Design

2013 ◽  
Author(s):  
Gideon J. Smit ◽  
Johannes Knoetze ◽  
Francois Steyn ◽  
Charle W. Rousseau ◽  
Erhardt R. De Kock
Keyword(s):  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Motor Design ◽  
Solid Rocket

In-flight S-band telemetry attenuation by ionized solid rocket motor plumes at high altitude

2019 ◽  
Vol 165 ◽  
pp. 373-381
Author(s):  
Kiyoshi Kinefuchi ◽  
Hiroyuki Yamaguchi ◽  
Mineko Minami ◽  
Koichi Okita ◽  
Takashi Abe
Keyword(s):  
High Altitude ◽  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Solid Rocket

Solid rocket motor design employing an efficient performance matching approach

2018 ◽  
Vol 233 (11) ◽  
pp. 4052-4065 ◽  
Author(s):  
Wu Zeping ◽  
Wang Donghui ◽  
Wang Wenjie ◽  
Patrick N Okolo ◽  
Zhang Weihua
Keyword(s):  
Rocket Motor ◽  
Test Cases ◽  
Optimization Approach ◽  
Solid Rocket Motor ◽  
One Dimensional ◽  
Time Stepping ◽  
Efficient Performance ◽  
Motor Design ◽  
Solid Rocket ◽  
Performance Validation

Solid rocket motor design matching the thrust requirement of the overall vehicle has become an exigent task. In the present research, an efficient performance matching optimization approach is proposed and applied to the solid rocket motor design. To obtain reliable solid rocket motor designs, refined performance evaluation is accomplished successfully based on the coupling of the level set grain burnback analysis and one-dimensional ballistic simulation by the time-stepping algorithm. Due to the heavy computing burden of the coupled performance solver, a novel progressive matching optimization approach is proposed. This approach depends on partial but not full-burn thrust profile to eliminate inferior candidates, predict superior candidates, advance the simulation and drive the candidates converging to the specified performance. Validation of the proposed solid rocket motor design approach is carried out by two test cases possessing different thrust requirements, and results indicate that the proposed approach is practical and efficient.

scholarly journals Solid Rocket Motor Design using a Low-Dimensional Fluid Model.

2019 ◽  
Author(s):  
Miguel Alejandro Aguilo Valentin ◽  
Steven W. Bova ◽  
David R. Noble
Keyword(s):  
Fluid Model ◽  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Motor Design ◽  
Solid Rocket ◽  
Low Dimensional

Fresh approach to solid rocket motor design

1995 ◽  
Vol 11 (4) ◽  
pp. 579-582 ◽  
Author(s):  
I. I. Velichko ◽  
N. A. Obukhov ◽  
V. S. Shishkin
Keyword(s):  
Rocket Motor ◽  
Solid Rocket Motor ◽  
Motor Design ◽  
Solid Rocket
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