Evaluation of altitude compensating nozzle concepts for RLV

Author:

Muss J.1,Nhuyen T.1,Reske E.2,McDaniels D.2,Muss J.1,Nhuyen T.1,Reske E.2,McDaniels D.2

Affiliation:

1. GenCorp Aerojet, Azusa, CA

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

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 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. Assessment of Aerospike Nozzle for Single-Stage to Orbit Flight;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23

2. Numerical Analysis of Film Cooling in Advanced Rocket Nozzles;AIAA Journal;2009-11

3. Film Cooling Effect on Dual-Bell Nozzle Flow Transition;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

4. Thermo-Fluid-Dynamics Analysis of Film Cooling in Overexpanded Rocket Nozzles;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

5. Numerical Study of Transition Between the Two Operating Modes of Dual-Bell Nozzles;38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2002-07-07

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