The experiments for the enhancement of regression rate of hybrid rocket fuel
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/content/pdf/10.1007/BF02984273.pdf
Reference14 articles.
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2. George, P., Krishnan, S., Varkey, P. M, Ravindran, M. and Ramachandran, L., 1998, “Fuel Regression Rate Enhancement Studies In HTPB/ GOX Hybrid Rocket Motors,” AIAA paper 9835064, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
3. Humble, R. W., Henry, G. N. and Larson, W. J., 1995,Space Propulsion Analysis and Design, McGraw-Hill, Inc., Chap, 7.
4. Knuth, W. H., Chiaverini, M. J., Gramer, D. J. and Sauer, J. A., 1998, “Experimental Investigation of A Vortex-Driven High-Regression Rate Hybrid Rocket Engine,” AIAA paper 98–3348, 34th- AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
5. Knuth, W. H., Chiaverini, M. J., Gramer, D. J. and Sauer, J. A., 1998, “Development and Testing of a vortex-driven, High-regression Rate Hybrid Rocket Engine,” AIAA paper 98–3507, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
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