Numerical analysis of fuel regression rate distribution characteristics in hybrid rocket motors with different fuel types
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering,General Materials Science
Link
http://link.springer.com/content/pdf/10.1007/s11431-013-5251-0.pdf
Reference24 articles.
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2. Tsohas J, Appel B, Rettenmaier A, et al. Development and launch of the purdue hybrid rocket technology demonstrator. AIAA Paper 2009-4842, 2009
3. Taylor F W, Howard R. Dream chaser for space transportation: Tourism, NASA and military integrated on a Atlas V. AIAA Paper 2008-7837, 2008
4. Evans B, Boyer E, Kuo K K, et al. Hybrid rocket investigations at penn state university’s high pressure combustion laboratory: Overview and recent results. AIAA Paper 2009-5349, 2009
5. Rao D L, Cai G B, Zhu H, et al. Design and optimization of variable thrust hybrid rocket motors for sounding rockets. Sci China Tech Sci, 2012, 55: 125–135, doi: 10.1007/s11431-011-4597-4
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