Vinci Engine Development Testing, a Summary of Turbine Testing Results

Author:

Brodin Staffan,Steen J.,Ljungkrona I.,Edin N.,Laumert B.

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. L. Helmers, J. Steen, I. Ljungkrona, S. Brodin, R. Johnsson, "Vinci LOX turbine aero design is described in:Turbine Design and Performance of Turbines in Expander Cycle Engine: The Vinci LOX turbine", 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and theInternationalInstitute of Space Law,Bremen,Sep. 29-3, 2003,IAC-03-S.3.05

2. A Mean Line Prediction Method for Axial Flow Turbine Efficiency

3. B.Goirand,P.Alliot,J-LBarthoulot&C.Bonhomme,"TestingthefirstfuelturbopumpoftheVinciEngine", 39thAIAA/ASME/SAE/ASEE Joint propulsionconf. and exhibit 20-23 July 2003, Huntsville, Alabama, AIAA 2003-5069.

4. K. Schäfer & H. Zimmerman, "Altitude simulation bench for VINCI Engine", 39thAIAA/ASME/SAE/ASEE Jointpropulsion conf.and exhibit20-23 July2003,Huntsville,Alabama, USA,AIAA2003-5043.

Cited by 2 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. Advanced Strategic Planning and Capability Identification in Order to Develop a Liquid Hydrogen Turbopump;Applied Mechanics and Materials;2014-06

2. A Transient Model of the VINCI Cryogenic Upper Stage Rocket Engine;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

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