Approximation Model Building for Reliability & Maintainability Characteristics of Reusable Launch Vehicles
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Roger A. Lepsch | Resit Unal | Richard W. Brown | W. Douglas Morris | N. H. White | Nancy H. White | R. Unal | W. Morris | R. Lepsch | Richard W. Brown
[1] Roger A. Lepsch,et al. Response Surface Model Building and Multidisciplinary Optimization Using D-Optimal Designs , 1998 .
[2] Douglas O. Stanley,et al. Dual-fuel propulsion in single-stage Advanced Manned Launch System Vehicle , 1995 .
[3] J. J. Griffin. Whole life cost studies: A defence management perspective , 1988 .
[4] T. W. Layne,et al. A Comparison of Approximation Modeling Techniques: Polynomial Versus Interpolating Models , 1998 .
[5] Raphael T. Haftka,et al. Response surface approximations for structural optimization , 1996 .
[6] Andrew Booker,et al. Design and analysis of computer experiments , 1998 .
[7] W. D. Morris,et al. Defining Support Requirements During Conceptual Design of Reusable Launch Vehicles , 1995 .