Multidisciplinary Design Optimization Approach for a Small Solid Propellant Launch Vehicle Conceptual Design Using Hybrid Simulated Annealing
International conference; 2nd, Mechanical and aerospace engineering; (ICMAE) 2011) ; 2011 ; Bangkok, Thailand
2012-01-01
7 pages
Includes bibliographical references and index.
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2013
|