Application of Taguchi methods to propulsion system optimization forSSTO vehicles
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
2. Old Dominion University, Hampton, Virginia 23665
3. Pratt & Whitney, West Palm Beach, Florida 33410
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25485
Reference11 articles.
1. Advanced technologies for rocket single-stage-to-orbit vehicles
2. Single-stage-to-orbit propulsion technologies
3. 3Anon. "High Performance Oxygen/Hydrogen Engine Definition: Final Technical Report," Pratt & Whitney, FR-21119,West PalmBeach,FL, March 1990.
4. 4Phadke, S. M., Quality Engineering Using Robust Design, Prentice-Hall, Englewood Cliffs, NJ, 1989, pp.41-65.
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