Author:
Khan Taj Wali,Qamar Ihtzaz
Publisher
Springer Science and Business Media LLC
Reference16 articles.
1. Humble R., Space propulsion analysis and design, 2nd ed., The McGraw-Hill Companies, 1995.
2. Rahman S.A, Hebert B.J., Large liquid rocket testing — strategies and challenges, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Tucson, Arizona, 2005, DOI: AIAA-2005-3564.
3. Han Y.M, Kim S.H., Seo S., Lee K.J, Kim J.G., Seol W.S., Development of sub-scale combustor for a liquid rocket engine using swirl injector with external mixing. Journal of the Korean Society for Aeronautics and Space Science, 2004, 32(10): 102–111.
4. Peretz A., Einav O., Hashmonay B.A, Birnholz A., Sobe Z., Development of a laboratory-scale system for hybrid rocket motor testing. Journal of Propulsion and Power, 2011, 27(1): 190–196.
5. Andrés F., Alejandro U.P.J., Fabio R., Design, manufacture, assembly and testing of a liquid (LOX and gasoline) rocket motor for a vehicle with stratospheric apogee in colombia: The SUA II engine, 7th European Conference for Aeronautics and Space Sciences, Milano, 2017. DOI: https://doi.org/10.13009/EUCASS2017-282.
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