Rocket-based combined cycle propulsion technology for access-to-space applications-Reference-Cited by-同舟云学术

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Rocket-based combined cycle propulsion technology for access-to-space applications

Published:1999-08-22 Issue: Volume: Page:
ISSN:
Container-title:9th International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Hueter Uwe¹

Affiliation:

1. NASA, Marshall Space Flight Center, Huntsville, AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-4925

Cited by 7 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. Drag reduction characteristics of recirculation flow at rocket base in an RBCC engine under ramjet/scramjet mode;Chinese Journal of Aeronautics;2023-12

2. Sea-Level Static Tests of Rocket–Ramjet Combined Cycle Engine Model;Journal of Propulsion and Power;2021-05

3. Numerical modeling and experimental investigation on the rocket-ejector system with limited mixer length;Acta Astronautica;2021-05

4. Space traffic management: towards safe and unsegregated space transport operations;Progress in Aerospace Sciences;2019-02

5. Comparison of Turbine-Based Combined-Cycle Engine Flowpaths;12th AIAA International Space Planes and Hypersonic Systems and Technologies;2003-12-15

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