| Entry, descent and landing systems analysis study: Phase 1 report AM DwyerCianciolo, JL Davis, DR Komar, MM Munk, JA Samareh, ... | 126 | 2010 |
| Aerodynamic configuration design using response surface methodology analysis WC Engelund, DO Stanley, RA Lepsch, MM McMillin, R Unal NASA STI/Recon Technical Report A 94, 10718, 1993 | 87 | 1993 |
| Comparison of two multidisciplinary optimization strategies for launch-vehicle design RD Braun, RW Powell, RA Lepsch, DO Stanley, IM Kroo Journal of Spacecraft and Rockets 32 (3), 404-410, 1995 | 84 | 1995 |
| NASA’s exploration systems architecture study D Stanley, S Cook, J Connolly, J Hamaker, M Ivins, W Peterson, J Geffre, ... NASA Final Report, TM-2005-214062, 2005 | 71 | 2005 |
| Approximation model building and multidisciplinary design optimization using response surface methods R Unal, R Lepsch, W Engelund, D Stanley 6th Symposium on Multidisciplinary Analysis and Optimization, 4044, 1996 | 65 | 1996 |
| Rocket-powered single-stage vehicle configuration selection and design DO Stanley, WC Engelund, RA Lepsch, M McMillin, KE Wurster, ... Journal of spacecraft and rockets 31 (5), 792-798, 1994 | 64 | 1994 |
| Propulsion system design optimization using the Taguchi method R Unal, DO Stanley, CR Joyner IEEE Transactions on Engineering Management 40 (3), 315-322, 1993 | 57 | 1993 |
| NASA strategic framework for on-demand air mobility B Holmes, R Parker, D Stanley, P McHugh, L Garrow, P Masson, J Olcott NASA Contractor Report NNL13AA08B, National Institute of Aerospace, Hampton, VA, 2017 | 40 | 2017 |
| Application of Taguchi methods to dual mixture ratio propulsion system optimization for SSTO vehicles D STANLEY, R Unal, C Joyner 30th Aerospace Sciences Meeting and Exhibit, 213, 1992 | 31 | 1992 |
| Dual-fuel propulsion in single-stage advanced manned launch system vehicle RA Lepsch Jr, DO Stanley, R Unal Journal of Spacecraft and Rockets 32 (3), 417-425, 1995 | 27 | 1995 |
| Application of Taguchi methods to propulsion system optimization forSSTO vehicles DO Stanley, R Unal, CR Joyner Journal of Spacecraft and Rockets 29 (4), 453-459, 1992 | 26 | 1992 |
| Single-stage-to-orbit—A step closer DC Freeman Jr, DO Stanley, CJ Camarda, RA Lepsch, SA Cook Acta Astronautica 37, 87-94, 1995 | 25 | 1995 |
| Conceptual design of a fully reusable manned launch system DO Stanley, TA Talay, RA Lepsch, WD Morris, KE Wurster Journal of Spacecraft and Rockets 29 (4), 529-537, 1992 | 24 | 1992 |
| Advanced technologies for rocket single-stage-to-orbit vehicles AW Wilhite, LB Bush, CI Cruz, RA Lepsch, WD Morris, DO Stanley, ... Journal of Spacecraft and Rockets 28 (6), 646-651, 1991 | 22 | 1991 |
| A space transportation architecture for the future D Stanley Acta astronautica 47 (2-9), 265-274, 2000 | 21 | 2000 |
| Design options for advanced manned launch systems DC Freeman, TA Talay, DO Stanley, RA Lepsch, AW Wilhite Journal of Spacecraft and Rockets 32 (2), 241-249, 1995 | 21 | 1995 |
| Multidisciplinary Optimization Strategies for Launch Vehicle Design RD Braun, RW Powell, RA Lepsch, DO Stanley, IM Kroo AIAA paper, 7-9, 1994 | 19 | 1994 |
| Design for quality using response surface methods: an alternative to Taguchi's parameter design approach R Unal, DO Stanley, W Engelund, R Lepsch Engineering Management Journal 6 (3), 40-48, 1994 | 16 | 1994 |
| An adaptive real time atmospheric prediction algorithm for entry vehicles J Wagner, A Wilhite, D Stanley, R Powell 3rd AIAA Atmospheric Space Environments Conference, 3200, 2011 | 15 | 2011 |
| Technology and staging effects on two-stage-to-orbit systems AW Wilhite, WC Engelund, DO Stanley, JC Naftel, RA Lepsch, LB Bush, ... Journal of Spacecraft and Rockets 31 (1), 31-38, 1994 | 15 | 1994 |
