Application of Taguchi methods to dual mixture ratio propulsion system optimization for SSTO vehicles
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. Old Dominion University, Norfolk, VA
3. Pratt and Whitney Group, West Palm Beach, FL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-213
Reference11 articles.
1. Single-stage-to-orbit propulsion technologies
2. "HighPerformanceOxygenEIydmgenEngineDefinition: FinalTechnicalRe~"Pratt&Whihley,USAFContract - MI-87-C-0073,March 1990.
3. Phadke,S.M.,QualitvEneineerineUsineRobustDesim, PrenticeHall,EnglewoodCliffs,NewJersey,1989.
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