Operation Analysis of a New Ignition System for SCRAM Jet Engine
Author:
Affiliation:
1. Department of Aerospace Engineering, National Defense Academy
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/astj/19/0/19_JSASS-D-19-00019/_pdf
Reference56 articles.
1. 1) Curran, E. T. and Murthy, S. N. B.: Scramjet Propulsion, Prog. Astro. Aero., 189 (2001), pp. 369-1293.
2. 2) Voland, R. T., Auslender, A. H., Smart, M. K., Roudakova, A. S., Semenov, V. L. and Kopchenov, V.: CIAM/NASA Mach 6.5 Scramjet Flight and Ground Test, AIAA Paper 99-4848, 1999.
3. 3) Moses, P. L., Rausch, V. L., Nguyen, L. T. and Hill, J. R.: NASA Hypersonic Flight Demonstrators - Overview, Status, and Future Plans, Acta Astronautica, 55 (2004), pp. 619-630.
4. 4) Boyce, R. R., Tirtey, S. C., Brown, L., Creagh, M. and Ogawa, H.: SCRAMSPACE: Scramjet-based Access-to-Space Systems, AIAA Paper 2011-2297, 2011.
5. 5) Falempin, F.: French Contribution to the Development of High-speed Airbreathing Propulsion Technology, ISABE 2011-1514, 2011.
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