Nano Archive

The Miniature Pressure Sensor for Monitoring and Diagnostics of Rocket-Space Engineering in Conditions of Mechanical and Thermal Effects

Barulina, M.A. and Dzhashitov, V.E. and Pankratov, V.M. (2009) The Miniature Pressure Sensor for Monitoring and Diagnostics of Rocket-Space Engineering in Conditions of Mechanical and Thermal Effects. Journal of NANO and MICROSYSTEM TECHNIQUE (6).

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Official URL: http:// www.microsystems.ru

Abstract

The connected mathematical models of non-stationary thermal processes, of the thermoelastic strained-de­formed condition and strength of the miniature pressure sensor applied to monitoring and diagnostics of a con­dition of space-rocket engineering and functioning in conditions mechanical and thermal impacts are constructed. Are solved problems of calculation and the analysis of non-stationary temperature fields of the sensor and its thermoelastic is strained-deformed condition. Estimations of strength of the sensor are received at mechanical and thermal effects. The computer experiments verifying adequacy and functionability mathematical, algorith­mic and the software are conducted, quantitative estimations are received and recommendations on maintenance of effective functioning the miniature pressure sensor are developed. Keywords: miniature pressure sensor, temperature fields, strained-deformed condition, finite-element mathe­matical model, mechanical and thermal effects.

Item Type:Article
Additional Information:Full text is in Russian
ID Code:10163
Deposited By:Prof. Alexey Ivanov
Deposited On:08 Dec 2010 23:39
Last Modified:09 Dec 2010 09:29

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