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Design Problems of Ballistic Missile Tank Structures: Simplified Analysis of the Effects of Axial Compression and Internal Pressure on Structural Stability

D.S. Houghton M.Sc.(Eng.), A.M.I.Mech.E., A.F.R.Ae.S. (Royal Military College of Science, Shrivenham.)
D.J. Johns M.Sc.(Eng.), M.I.Ae.S. (Department of Aircraft Design, The College of Aeronautics, Cranfield.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 July 1961

57

Abstract

The in‐flight design problems of ballistic missile fuel tank structures are examined and simplified analyses are presented.

Citation

Houghton, D.S. and Johns, D.J. (1961), "Design Problems of Ballistic Missile Tank Structures: Simplified Analysis of the Effects of Axial Compression and Internal Pressure on Structural Stability", Aircraft Engineering and Aerospace Technology, Vol. 33 No. 7, pp. 188-192. https://doi.org/10.1108/eb033430

Publisher

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MCB UP Ltd

Copyright © 1961, MCB UP Limited

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