Weights Analysis of Space Launch Vehicles in an Advanced Engineering Environment-Reference-Cited by-同舟云学术

Weights Analysis of Space Launch Vehicles in an Advanced Engineering Environment

Published:2004-08-30 Issue: Volume: Page:
ISSN:
Container-title:10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
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Author:

Jiang Xun,Gage Peter,Vander Kam Jeremy,Qu Min

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4562

Reference6 articles.

1. 1Monell, D, Mathias, D. Reuther, J., and Garn M. "The Advanced Engineering Environment (AEE) Project for NASA's NGLTProgram," AIAA 2004-0202, 42nd AerospaceSciences Meeting,Reno, NV,Jan.2004

2. 2Vander Kam, J., and Gage. P, "A Data Model for Evaluating Reusable Launch Vehicle Concepts,"2003-1330, 41st AerospaceSciences Meeting, Reno, NV,Jan.2003

3. 3Qu, M, Sohn, J., Gage, P., and Bradford B. "Generalized Vehicle Performance Closure Model for Two-Stage-to-Orbit ReusableLaunch Vehicles,"AIAA 2004-1221, 42nd AerospaceSciences Meeting, Reno,NV,Jan.2004

4. Utilizing air-turborocket and rocket propulsion for a single-stage-to-orbit vehicle

5. 12Lau, E, Wong, J., Vander Kam, J., Jiang,X.,Palmer, G. and Gage, P. "LVL Editor: A Graphical Tool for Visualizing and Managing Data in an Engineering Component Hierarchy," AIAA 2004-1173, 42nd Aerospace Sciences Meeting, Reno, NV, Jan. 2004

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