An approach for space launch vehicle conceptual design and multi-attribute evaluation
- 1 March 2013
- journal article
- Published by Elsevier BV in Aerospace Science and Technology
- Vol. 25 (1), 65-74
- https://doi.org/10.1016/j.ast.2011.12.008
Abstract
No abstract availableKeywords
This publication has 24 references indexed in Scilit:
- Simultaneous optimization of staging and trajectory of launch vehicles using two different approachesAerospace Science and Technology, 2011
- Optimal air-launching rocket design using system trades and a multi-disciplinary optimization approachAerospace Science and Technology, 2009
- Multidisciplinary design optimization of a small solid propellant launch vehicle using system sensitivity analysisStructural and Multidisciplinary Optimization, 2008
- Cost efficiency as design and selection criterion for future launch vehiclesActa Astronautica, 2005
- Low-cost management aspects for developing, producing and operating future space transportation systemsActa Astronautica, 2005
- Review of aerospace engineering cost modelling: The genetic causal approachProgress in Aerospace Sciences, 2004
- Analytic performance considerations for lifting ascent trajectories of winged launch vehiclesActa Astronautica, 2004
- A Fuzzy TOPSIS Method for Robot SelectionThe International Journal of Advanced Manufacturing Technology, 2003
- A new efficient method of multi-stage solid rocket optimizationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Comparisons of rocket and air-breathing vehicle concepts for earth-to-orbit transportarionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990