Flow phenomena in advanced rocket nozzles - The plug nozzle
Author:
Affiliation:
1. DLR, Hardthausen, Germany
2. Daimler-Benz Aerospace, Space Infrastructure, Ottobrunn, Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3522
Reference21 articles.
1. Gross, G. W. "Performance Analysis of AerospikeRocket Engines",NASA STAR Technical Report Issue 3, NASA Marshall Space Flight Center, 1973
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