Chapter 6: Evaluation of Cardiothermal Model Prediction of Simulated Lunar Extravehicular ActivityFewer than 20 extravehicular activities were completed during the Apollo program. The lunar environment has consistent unknowns to address particularly that of suited performance in partial gravity. The moon has altered gravity that is 1/6th that of Earth’s. This study is focused to investigate validation of the regression techniques identified in subsequent chapters and look to improve predictive outcomes during simulated lunar EVA tasks. Heart rate predictions of metabolic energy expenditure are investigated to predict workload throughout simulated lunar EVA conducted in the active response gravity offload system (ARGOS) with in the NASA Mark III space suit. Heart rate variability metrics are utilized to identify periods of high workload. Continually, the lunar offload capacity is further characterized to aid in improving the cardiothermal prediction models including predictions of core temperature, skin temperature and heat storage using heart rate, metabolic rates and suit thermal data during the simulated EVA. The outcome of this model provides an application for future use in contingency predictions of energy expenditure during Lunar EVAs and provide a suite of instrumentation to predict workload during training scenarios.
Document ID
20210024108
Acquisition Source
Johnson Space Center
Document Type
Thesis/Dissertation
Authors
Bradley Hoffmann (Wyle (United States) El Segundo, California, United States)
Date Acquired
November 8, 2021
Publication Date
November 29, 2021
Publication Information
Publication: Evaluation of Heart Rate Variability and Cardiovascular Regulation to In-flight Workload and Thermal Stress
Publisher: University of North Dakota
Subject Category
Man/System Technology And Life Support
Funding Number(s)
CONTRACT_GRANT: NNJ15HK11B
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Simulated EVAHeart rate variabilitySpacesuit thermal regulationHuman thermal model