Multidisciplinary Cost and Performance Optimization of a Two Stage Liquid Propulsion Based Launch Vehicle-Reference-Cited by-同舟云学术

Multidisciplinary Cost and Performance Optimization of a Two Stage Liquid Propulsion Based Launch Vehicle

Published:2008-04-28 Issue: Volume: Page:
ISSN:
Container-title:15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
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Author:

LeMoyne Robert

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2642

Reference8 articles.

1. Anderson; Introductionto Flight; McGraw-Hill; NewYork; 1989.

2. Isakowitz; Space LaunchSystems; AIAA; WashingtonD.C.; 1991.

3. Johanson; Cost OptimizationofLiquid Fuel Rockets; UniversityofMichigan(Mechanical Engineering 555); [http://www.optimaldesign.org/archive.html]; 566-88-01; 1988.

4. Larson, Wertz; Space Mission Analysis and Design; MicrocosmPress; Torrance, Ca; 1992.

5. LeMoyne; AIAA2005-3204Fundamental Architectural Analysis ofa Subsonic SeparationLowEarth Orbit LaunchVehicle.

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