Optimal design of hybrid rocket motor powered vehicle for suborbital flight-Reference-Cited by-同舟云学术

Optimal design of hybrid rocket motor powered vehicle for suborbital flight

Published:2013-03 Issue:1 Volume:25 Page:114-124
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Cai Guobiao,Zhu Hao,Rao Dalin,Tian Hui

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. D. Altman, Hybrid rocket development history, in: 27th AIAA/SAE/ASME/ASEE Joint Propulsion Conference, AIAA Paper No. 91-2515, Sacramento, June 24–26, 1991.

2. J.P. Arves, H. Stephen Jones, Overview of hybrid sounding rocket program, in: 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper No. 1997-2799, Seattle, July 6–9, 1997.

3. Design optimization of a space launch vehicle using a genetic algorithm;Bayley;Journal of Spacecraft and Rockets,2008

4. Scale effect of fuel regression rate in hybrid rocket motor;Cai;Aerospace Science and Technology,2013

5. Acoustics vortex shedding and low-frequency dynamics interaction in an unstable hybrid rocket;Carmicino;Journal of Propulsion and Power,2009

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