Failure pressure estimations on a solid propellant rocket motor with a circular perforated grain-Reference-Cited by-同舟云学术

Failure pressure estimations on a solid propellant rocket motor with a circular perforated grain

Published:1999-12 Issue:14-15 Volume:76 Page:955-963
ISSN:0308-0161
Container-title:International Journal of Pressure Vessels and Piping
language:en
Short-container-title:International Journal of Pressure Vessels and Piping

Author:

Renganathan K.,Nageswara Rao B.,Jana M.K.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference10 articles.

1. Renganathan K, Nageswara Rao B. Analysis of a strip biaxial tension specimen of a HTPB based propellant material. VSSC Technical Report No. VSSC/SDA/TR-002/1999.

2. Rajan M, Mohandas CV, Sree Kumar KV. On the properties of HTPB-based PS3-propellant. Propellant Group, Vikram Sarabhai Space Centre, Trivandrum, India. Report No. PCM/PRG/05/85, April 1985.

3. Bursting pressure of cylindrical and spherical vessels;Svensson;Trans ASME J Appl Mech,1958

4. The ultimate strength of thick walled cylinders subjected to internal pressure;Crossland;Engineering (London),1955

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