Design Optimization on Cost Basis Using Orthogonal Arrays

References

• 1995 . JMP Statistics and Graphics Guide , Cary , NC : SAS Institute Inc . Anon.
   Google Scholar
• Braun , R. D. , Powell , R. W. , Lepsch , R. A. , Stanley , D. O. and Kroo , I. M. 1995 . ). Comparison of two multidisciplinary optimization strategies for launch vehicle design . Journal of Spacecraft & Rockets , 32 ( 3 ) : 404 – 410 .
   Web of Science ®Google Scholar
• Eldred , C. H. , Powell , R. W. and Stanley , D. O. 1993 . Single stage rocket options for future launch vehicles AIAA Paper 93–4162
   Google Scholar
• Engelund , W. C. , Stanley , D. O. , McMillin , M. L. and Unal , R. 1993 . Aerodynamic configuration design using response surface methodology analysis 1 – 11 . AIAA Paper 93–3967
   Google Scholar
• Fabrycky , W. J. and Blanchard , B. S. 1991 . Life Cycle Cost and Economic Analysis , Englewood Cliffs , NJ : Prentice Hall .
   Google Scholar
• Freeman , D. C. , Talay , T. A. , Stanley , D. O. , Lepsch , R. A. and Wilhite , A. W. 1995 . ). Design options for advanced manned launch systems . Journal of Spacecraft and Rockets , 32 ( 2 ) : 241 – 249 .
   Web of Science ®Google Scholar
• Kackar , R. 1989 . Off-line quality control, parameter design and Taguchi method . Journal of Quality Technology , 17 ( 4 ) : 176 – 188 .
   Google Scholar
• Lepsch , R. A. , Stanley , D. O. and Unal , R. 1995 . ). Dual-fuel propulsion in a single stage advanced manned launch vehicle . Journal of Spacecraft and Rockets , 32 ( 3 ) : 417 – 425 .
   Web of Science ®Google Scholar
• Lepsch , R. A. , Stanley , D. O. , Cruz , C. I. and Morris , S. J. 1991 . ). Utilizing air-turborocket and rocket rropulsion for a single-stage-to-orbit vehicle . Journal of Spacecraft and Rockets , 28 ( 5 ) : 560 – 566 .
   Web of Science ®Google Scholar
• Moore , A. A. , Braun , R. B. and Powell , R. W. The infusion of cost elements into the multidisciplinary optimization of space transportation systems . Proceedings of ISPA Annual Conference . pp. 164 – 182 .
   Google Scholar
• Montgomery , D. C. 1991 . Design and Analysis of Experiments , NJ : John Wiley and Sons .
   Google Scholar
• Olds , J. R. 1992 . Tshe suitability of selected multidisciplinary design optimization techniques to conceptual aerospace vehicle design 1 – 12 . AIAA Paper 92–4791
   Google Scholar
• Phadke , S. M. 1989 . Quality Engineering Using Robust Design , Englewood Cliffs , NJ : Prentice Hall .
   Google Scholar
• Stanley , D. O. , Unal , R. and Joyner , R. 1992 . ). Application of Taguchi methods to dual-mixture ratio propulsion system optimization for SSTO vehicles . Journal of Spacecraft and Rockets , 29 ( 4 ) : 453 – 459 .
   Web of Science ®Google Scholar
• Stanley , D. O. , Engelund , W. C. , Lepsch , R. A. , McMillin , M. L. , Wurster , K. E. , Powell , R. W. , Guinta , A. A. and Unal , R. 1994 . ). Rocket-powered single-stage vehicle configuration selection and design . Journal of Spacecraft and Rockets , 31 ( 5 ) : 792 – 798 .
   Web of Science ®Google Scholar
• Taguchi , G. and Konishi , S. 1987 . Orthogonal arrays and linear graphs , Dearborn , MI : American Supplier Institute Inc. .
   Google Scholar
• Unal , R. , Braun , R. , Moore , A. and Lepsch , R. Design optimization on cost basis using Taguchi's orthogonal arrays . Proceedings of the American Society for Engineering Management National Conference . pp. 17 – 21 .
   Google Scholar
• Unal , R. , Bush , L. B. , Ball , J. M. and Lindegren , K. R. 1993 . ). Aerobrake parametric optimization study . Journal of Parametrics , 13 ( 1 ) : 51 – 65 .
   Google Scholar
• Venter , G. , Haftka , R. and Starnes , J. Jr. Construction of response surfaces for design optimization applications . Proceedings of the 6th Annual AIAA/USAF/ NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization . pp. 548 – 564 .
   Google Scholar
• Wilhite , A. W. , Bush , L. B. , Cruz , C. I. , Lepsch , R. A. , Morris , W. D. , Stanley , D. O. and Wurster , K. E. 1991 . ). Advanced technologies for rocket-powered single-stage-to-orbit vehicles . Journal of Spacecraft and Rockets , 28 ( 6 ) : 646 – 651 .
   Web of Science ®Google Scholar
• Wille , R. 1990 . ). Landing gear weight optimization using Taguchi analysis . Society of Allied Weight Engineers (SAWE)-Paper , 1966 : 11
   Google Scholar