Synerjet for Earth/orbit propulsion - Revisiting the 1966 NASA/Marquardt composite (airbreathing/rocket) propulsion system study (NAS7-377)

Author:

Escher William1

Affiliation:

1. NASA, Washington, DC

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. (Reprintedinthe Institut fuer Raumfahrtantriebe 1984 publication reviewingits activitiesforthe period 1970-1984)

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

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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