Comparison of two multidisciplinary optimization strategies for launch-vehicle design
- 1 May 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 32 (3), 404-410
- https://doi.org/10.2514/3.26629
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- 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
- Rocket-powered single-stage vehicle configuration selection and designJournal of Spacecraft and Rockets, 1994
- Multidisciplinary optimization methods for aircraft preliminary designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Optimization of coupled systems - A critical overview of approachesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Single stage rocket options for future launch vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Post-optimality analysis in aerospace vehicle designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Development of the quasi-procedural method for use in aircraft configuration optimizationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Advanced technologies for rocket single-stage-to-orbit vehiclesJournal of Spacecraft and Rockets, 1991
- Frontiers in Engineering OptimizationJournal of Mechanical Design, 1983