Synerjet for Earth/orbit propulsion - Revisiting the 1966 NASA/Marquardt composite (airbreathing/rocket) propulsion system study (NAS7-377)
Author:
Affiliation:
1. NASA, Washington, DC
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3040
Reference11 articles.
1. (Reprintedinthe Institut fuer Raumfahrtantriebe 1984 publication reviewingits activitiesforthe period 1970-1984)
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1. Component-level weight analysis for RBCC engines;Defense and Space Programs Conference and Exhibit - Critical Defense and Space Programs for the Future;1997-08-22
2. Application of a new economic analysis tool to a two-stage-to-orbit RBCC launch vehicle design;6th Symposium on Multidisciplinary Analysis and Optimization;1996-08-22
3. Fan integration into the hypersonic combined-cycle engine - Background, rationale and candidate technical approaches;32nd Joint Propulsion Conference and Exhibit;1996-07-01
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