Design, Fabrication and Test of the RL60 Fuel Turbopump
Author:
Affiliation:
1. Ishikawajima Harima Heavy Industries Co., Ltd.
2. Pratt & Whitney Space Propulsion
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5073
Reference5 articles.
Cited by 4 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. Cryogenic Tribology of High-Speed Bearings and Shaft Seals in Liquid Hydrogen;Tribology Online;2011
2. Improvement of Durability of Hybrid Ceramic Ball Bearings in Liquid Hydrogen at 3 Million DN (120,000 rpm);Tribology Online;2010
3. RL60 - The Next Step in the Evolution of Upperstage Engines;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26
4. RL60 Demonstrator Engine Design, Manufacturing, and Test;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26
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