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Use of Longeron Anchored Cables in Multilobed Liquid Booster Tanks

Published online by Cambridge University Press:  04 July 2016

Bertram Klein
Bertram Klein*
Affiliation:
Space Systems Division, Hughes Aircraft, El Segundo, California
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Extract

The use of multilobed pressure vessels is not new. Such structures have been used in civil engineering applications for many years. It has been recognised that substantial weight savings are possible by reducing the radius of curvature by lobing. Usually the resulting discontinuity stresses at the junctions of the lobes have been balanced by attaching flat plates.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 69 , Issue 654 , June 1965 , pp. 414 - 417
Copyright
Copyright © Royal Aeronautical Society 1965

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References

1.Sterett, J. B. Shell Stability Problems in the Design of Large Space Vehicle Boosters. NASA TN D-1510, pp 57-66, December 1962.Google Scholar
2.Blumrich, J. F. Multicell Structures. Space Aeronautics, pp 86-89, January 1963.Google Scholar
3.Runyan, H. L. and Leonard, R. W.Research, Design Considerations, and Technological Problems of Structures for Launch Vehicles. Proceedings of the NASA - University Conference on the Science and Technology of Space Exploration. Chicago, Vol. 2, pp 487–498, November 1962.Google Scholar