A Risk-Based Approach for Aerothermal/TPS Analysis and Testing

Abstract

The current status of aerothermal and thermal protection system modeling for civilian entry missions is reviewed. For most such missions, the accuracy of our simulations is limited not by the tools and processes currently employed, but rather by reducible deficiencies in the underlying physical models. Improving the accuracy of and reducing the uncertainties in these models will enable a greater understanding of the system level impacts of a particular thermal protection system and of the system operation and risk over the operational life of the system. A strategic plan will be laid out by which key modeling deficiencies can be identified via mission-specific gap analysis. Once these gaps have been identified, the driving component uncertainties are determined via sensitivity analyses. A Monte-Carlo based methodology is presented for physics-based probabilistic uncertainty analysis of aerothermodynamics and thermal protection system material response modeling. These data are then used to advocate for and plan focused testing aimed at reducing key uncertainties. The results of these tests are used to validate or modify existing physical models. Concurrently, a testing methodology is outlined for thermal protection materials. The proposed approach is based on using the results of uncertainty/sensitivity analyses discussed above to tailor ground testing so as to best identify and quantify system performance and risk drivers. A key component of this testing is understanding the relationship between the test and flight environments. No existing ground test facility can simultaneously replicate all aspects of the flight environment, and therefore good models for traceability to flight are critical to ensure a low risk, high reliability thermal protection system design. Finally, the role of flight testing in the overall thermal protection system development strategy is discussed.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2007
Accession Number
ADA476515

Entities

People

  • Deepak Bose
  • Jay H. Grinstead
  • Michael J. Wright

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Boundary Layer
  • Chemical Reactions
  • Computational Fluid Dynamics
  • Computational Science
  • Flight Testing
  • Fluid Dynamics
  • Gas Surface Interactions
  • Heat Transfer
  • Information Science
  • Materials
  • Measurement
  • Regression Analysis
  • Reliability
  • Simulations
  • Test Facilities
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Aviation Safety Risk Assessment.
  • Computational Modeling and Simulation