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SOLROCK

Projekter: Projekt › Forskning

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Beskrivelse

The goal of this project was to develop a procedure for reliable structural analysis and service life
estimation of a solid rocket motor grain.
I did structural stress analyses of a full-scale model of a solid propellant rocket motor under actual
loading histories. An accurate material model of propellant was verified with including material ageing.

Funding 300.000 Euro
StatusAfsluttet
Effektiv start/slut dato01/01/2007 → 31/12/2010

ID: 145465905