An Automated Approach to Multidisciplinary System Design Optimization of Small Solid Propellant Launch Vehicles
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Publisher
IEEE
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http://xplorestaging.ieee.org/ielx5/10835/34153/01627501.pdf?arnumber=1627501
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Fast, robust and near-optimal approximation of GTO trajectories and payload capacities of multistage rockets;CEAS Space Journal;2019-03-15
2. Multidisciplinary Design Optimization Approach for a Small Solid Propellant Launch Vehicle Conceptual Design Using Hybrid Simulated Annealing;Applied Mechanics and Materials;2011-10-24
3. Multi-level of Fidelity Multi-Disciplinary Design Optimization of Small, Solid-Propellant Launch Vehicles;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2010
4. Multidisciplinary design optimization of a small solid propellant launch vehicle using system sensitivity analysis;Structural and Multidisciplinary Optimization;2008-07-15
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