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

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Review Article| July 01 1961

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.;

D.S. Houghton, M.Sc.(Eng.), A.M.I.Mech.E., A.F.R.Ae.S.

Royal Military College of Science, Shrivenham.

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D.J. Johns, M.Sc.(Eng.), M.I.Ae.S.

Department of Aircraft Design, The College of Aeronautics, Cranfield.

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Publisher: Emerald Publishing

Online ISSN: 2059-9366

Print ISSN: 0002-2667

1961

Aircraft Engineering (1961) 33 (7): 188–192.

https://doi.org/10.1108/eb033430

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

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1961

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