Use of the collaborative optimization architecture for launch vehicle design
- 22 August 1996
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Use of the collaborative optimization architecture for launch vehicle designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Multidisciplinary aerospace design optimization - Survey of recent developmentsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Dual-fuel propulsion in single-stage Advanced Manned Launch System VehicleJournal of Spacecraft and Rockets, 1995
- Problem Formulation for Multidisciplinary OptimizationSIAM Journal on Optimization, 1994
- Design for Quality Using Response Surface Methods: An Alternative to Taguchi's Parameter Design ApproachEngineering Management Journal, 1994
- 21st century space transportation system design approach - HL-20 personnel launch systemJournal of Spacecraft and Rockets, 1993
- Single stage rocket options for future launch vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Conceptual design of a fully reusable manned launch systemJournal of Spacecraft and Rockets, 1992
- Advanced technologies for rocket single-stage-to-orbit vehiclesJournal of Spacecraft and Rockets, 1991
- Optimum wing sizing of a single-stage-to-orbit vehicleJournal of Spacecraft and Rockets, 1983