Dual-fuel propulsion in single-stage Advanced Manned Launch System Vehicle

Author:

Lepsch Roger A.1,Stanley Douglas O.1,Unal Resit2

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681-0001

2. Old Dominion University, Norfolk, Virginia 23529

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Cited by 27 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. Multidisciplinary Design Optimization Approach for a Small Solid Propellant Launch Vehicle Conceptual Design Using Hybrid Simulated Annealing;Applied Mechanics and Materials;2011-10-24

2. 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

3. Using dual response surfaces to reduce variability in launch vehicle design: A case study;Reliability Engineering & System Safety;2006-04

4. Multi-Level, Multi-Objective and Multidisplinary Optimization Design of a Series of Launch Vehicles;55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law;2004-10-04

5. Liquid Rocket Thrust Chambers;2004-01-01

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