Verification of a Constraint Force Equation Methodology for Modeling Multi-Body Stage Separation-Reference-Cited by-同舟云学术

Verification of a Constraint Force Equation Methodology for Modeling Multi-Body Stage Separation

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Modeling and Simulation Technologies Conference and Exhibit
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Author:

Tartabini Paul¹,Roithmayr Carlos¹,Karlgaard Chris²,Toniolo Matt²,Pamadi Bandu¹

Affiliation:

1. NASA Langley Research Center

2. Analytical Mechanics Associates, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7039

Reference26 articles.

1. 2Taylor, R. T., and Alford, W. J., Jr. "A Wind Tunnel Investigation of the Carry Loads and Mutual Interference Effects of 1/40-Scale Models of theX-15 and B-52 Airplanes In Combination,"NASA TMX-184,1959.

2. 3Decker, J. P., and Wilhite, A. W. "Technology and Methodology of Separating Two Similar Size Aerospace Vehicles Within the Atmosphere,"AIAA Paper1975-29,Jan. 1975.

3. 5Decker, J. P., and Gera, J. "An Exploratory Study of Parallel-Stage Separation of Reusable Launch Vehicles," NASA TN D-4765,1968.

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3. Verification of a Constraint Force Equation Methodology for Modeling Multi-Body Stage Separation;AIAA Modeling and Simulation Technologies Conference and Exhibit;2008-06-15