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Probabilistic Assessment of Space Nuclear Propulsion System Nozzle PUBLIC ACCESS

[+] Author Affiliations
Ashwin R. Shah

Sverdrup Technology, Inc., Brookpark, OH

Richard D. Ball

Loral Aerosys, North Olmsted, OH

Paper No. 93-GT-381, pp. V03CT17A042; 11 pages
doi:10.1115/93-GT-381
From:
  • ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 3C: General
  • Cincinnati, Ohio, USA, May 24–27, 1993
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7892-7
  • Copyright © 1993 by ASME

abstract

Uncertainties associated with the design parameters of the Space Nuclear Propulsion System (SNPS) nozzle such as geometry, boundary conditions, material behavior, thermal and pressure loads, etc. are considered to assess its reliability. Preliminary assessment of the reliability is performed using NESSUS (Numerical Evaluation of Stochastic Structures Under Stress) computer code developed at NASA Lewis Research Center (LeRC). Probabilistic finite element analysis of the nozzle system is conducted and the sensitivity of reliability to the uncertainties in the random variables is quantified. For example the nozzle spatial geometry uncertainties have the most significant effect on the effective stress at low probabilities while the inner wall temperature has the most significant effect at higher probabilities.

Copyright © 1993 by ASME
This article is only available in the PDF format.

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