STABILITY BOUNDARIES OF LIQUID-PROPELLED SPACE VEHICLES WITH SLOSHING-Reference-Cited by-同舟云学术

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STABILITY BOUNDARIES OF LIQUID-PROPELLED SPACE VEHICLES WITH SLOSHING

Published:1963-07 Issue:7 Volume:1 Page:1583-1589
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

BAUER HELMUT F.¹

Affiliation:

1. NASA George C. Marshall Space Flight Center, Huntsville, Ala.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.1861

Reference9 articles.

1. Minorsky, N., Nonlinear Oscillations (D. Van Nostrand Co. Inc., Princeton, N. J.1962), Chap. 14, pp.329-335.

2. Minorsky, N., Nonlinear Oscillations (D. Van Nostrand Co. Inc., Princeton, N. J.1962), Chap. 16, pp.390-415.

3. March 1961;Melbourne W. G.

4. Fig. 2;For

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