Abstract
Finite element models (FEMs) of both small female and large male anthropomorphic test devices (ATDs) were developed and validated for use in occupant protection analysis for NASA human exploration spacecraft. These models are an important component of the suite of predictive tools which will be used to determine the risk of crew injuries due to spacecraft dynamic loadings. Physical ATD testing and correlation of test results to model predictions was performed to assess uncertainties associated with the FEMs ability to predict ATD responses to spaceflight loading environments. Both quantitative and qualitative metrics were used to assess model correlation quality. Model uncertainty factors were then determined for both small female and large male ATDs for each injury metric specified in NASA requirements.
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Notes
- 1.
A dimensionless measure of head acceleration during a 15-millisecond time interval, measured at the center of gravity of the dummy head.
- 2.
Consists of four neck criteria - neck tension-extension, neck tension-flexion, neck compression-extension, and neck compression-flexion.
References
Currie, N.J., Lawrence, C.: NASA Engineering and Safety Center Report: Crew Exploration Vehicle (Orion) Occupant Protection, NESC-RP-08-00469. NASA Langley Research Center, Hampton, VA (2012)
Somers, J., Newby, N., Wells, J.: Final NASA Panel Recommendations for Definition of Acceptable Risk of Injury due to Spaceflight Dynamic Events, TP-2015-218578. NASA Johnson Space Center. Houston, TX (2015)
National Aeronautics and Space Administration, Orion Multi-Purpose Crew Vehicle Program: Human-Systems Integration Requirements, MPCV 70024, Rev. C. NASA Johnson Space Center, Houston, TX (2012)
Somers, J., Gohmert, D., Brinkley, J.: Application of the Brinkley Dynamic Response Criterion to Spacecraft Transient Dynamic Events, TM-2013-217380-REV1. NASA Johnson Space Center. Houston, TX (2016)
Society of Automotive Engineers (SAE): Instrumentation for Impact Test–Part 1, Electronic Instrumentation, Standard J211/1. SAE International (2014)
Barbat, S., et al.: Objective rating metric for dynamic systems. Enhanced Safety of Vehicles, Seoul, Republic of Korea (2013)
International Organization for Standardization (ISO): Road vehicles–Objective rating metrics for dynamic systems, ISO/TR 16250:2013(E) (2013)
International Organization for Standardization (ISO): Road Vehicles–Objective Rating Metric for Non-Ambiguous Signals, ISO/TS 18571:2014(E) (2014)
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Currie-Gregg, N.J., Lawrence, C., Somers, J. (2018). Occupant Protection Modeling and Injury Prediction for NASA Human Exploration Spacecraft. In: Cassenti, D. (eds) Advances in Human Factors in Simulation and Modeling. AHFE 2017. Advances in Intelligent Systems and Computing, vol 591. Springer, Cham. https://doi.org/10.1007/978-3-319-60591-3_18
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DOI: https://doi.org/10.1007/978-3-319-60591-3_18
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