Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters
The principle goal of this paper is developing of Launch Vehicle Conceptual Design (LVCD) method based on combinational optimization of major design parameters. To this end, ten sub-algorithms will be presented in this design approach. Mass distribution of different stages to launch maximum payload...
| Main Authors: | , , |
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| Format: | Article |
| Language: | fas |
| Published: |
Aerospace Research Institute
2008-04-01
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| Series: | فصلنامه علوم و فناوری فضایی |
| Subjects: | |
| Online Access: | https://jsst.ias.ir/article_14358_b2753759d67cc69f2918fb5fe02ac509.pdf |