Application of Constraint Force Equation Methodology for Launch Vehicle Stage Separation

Bandu N. Pamadi; Paul V. Tartabini; Mathew D. Toniolo; Carlos M. Roithmayr; Christopher D. Karlgaard; Jamshid A. Samareh

doi:10.2514/1.a32048

journal article Jan 01, 2013

Application of Constraint Force Equation Methodology for Launch Vehicle Stage Separation

Bandu N. Pamadi Paul V. Tartabini Mathew D. Toniolo Carlos M. Roithmayr Christopher D. Karlgaard Jamshid A. Samareh

Journal of Spacecraft and Rockets Vol. 50 No. 1 pp. 191-205 · American Institute of Aeronautics and Astronautics (AIAA)

View at Publisher Save 10.2514/1.a32048

Topics

No keywords indexed for this article. Browse by subject →

References

26

[1]

Dillenius M. F. E. (1992)

[2]

Taylor R. T. (1959)

[3]

Hurley M. J. (1969)

[4]

10.2514/3.30393

[5]

10.2514/6.1975-29

[6]

Decker J. P. (1967)

[7]

Decker J. P. (1968)

[8]

Decker J. P. (1969)

[9]

Wilhite A. W. (1977)

[10]

10.2514/6.1986-195

[11]

10.2514/6.1990-223

[12]

Naftel J. C. (1993)

[13]

Murphy K. J. AIAA Paper (2004)

[14]

10.2514/1.17896

[15]

(1999)

[16]

Pamadi B. N. AIAA Paper (2006)

[17]

Reubush D. E. AIAA Paper (2003)

[18]

10.2514/1.51943

[19]

Kane T. R. (2005)

[20]

Schaechter D. B. Journal of the Astronautical Sciences (1988)

[21]

(1997)

[22]

(1981)

[23]

(1982)

[24]

(1981)

[25]

Bornemann W. E. (1983)

[26]

Angster S. (2011)

Metrics

4

Citations

26

References

Details

Published: Jan 01, 2013
Vol/Issue: 50(1)
Pages: 191-205

Authors

B

Bandu N. Pamadi