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Evaluation of Human Spaceflight-Related Tissue Weight Relief Using Whole Body Finite Element Model SimulationsTissue Weight Relief (TWR) is a physiological condition observed in human spaceflight. It not only impacts the injury biomechanics of soft tissue but also the physiological responses of the cardiovascular system both due to fluid redistribution and the effect of tissue-related transmural pressure on the large venous blood vessels. Understanding the effects of tissue weight relief is especially important because of the role it may play in understanding the cause of Space Associated Neuro-Ocular Syndrome (SANS). SANS can be characterized by a number of ocular changes which reduce visual acuity and SANS related symptoms occur in up to 51% of astronauts. A prevailing theory for the causation of SANS is that of headward (cephalad) fluid shift and a prolonged increase of Intracranial Pressure (ICP) similar to intracranial hypertension, which is not fully supported by the experimental data or astronaut symptom reporting. However, it is still believed that SANS is caused by a pressure change in the eye and the surrounding tissues. It has been proposed that TWR plays a substantial role in affecting internal pressures and fluid shifts in microgravity.

In this effort, two whole-body Finite Element (FE) models – Elemance and THUMS – are used to ascertain the microgravity-associated TWR of the musculature surrounding the lower body veins. Elemance and THUMS are physics-based computational models that have been validated and verified for several automotive and domestic applications, and as such, can simulate the relief of soft tissue weight due to changes in the gravitation vector. Specifically, the current effort modeled the transition of the gravitational vector from 1G to 0G, applied across the whole-body model in a supine position. For each 1G to 0G transition simulation, the lower body vein’s transmural pressure-time profile was extracted and averaged around the anterior portion of the thigh muscle. The ascertained transmural pressure changes from 1G to 0G transition are given in Figure 1 for the Elemance and the THUMS FE models. The transmural pressure changes of 10 mmHg and 21 mmHg are in the same order of magnitude as Lu’s value of 44 mmHg. It is to be noted that Lu implemented a 0D to 1D lumped parameter model and the Elemance and THUMS are 3D higher order computational models. This proof-of-concept approach demonstrates that TWR pressure can be adequately estimated with in silico techniques however, further in silico investigations need to be conducted to address the unique contributions to the transmural pressure from each of the computational models.
Document ID
20230001279
Acquisition Source
Glenn Research Center
Document Type
Poster
Authors
Caroline R Austin
(Glenn Research Center Cleveland, Ohio, United States)
R A Perkins
(Universities Space Research Association Columbia, Maryland, United States)
C A Gallo
(Glenn Research Center Cleveland, Ohio, United States)
B Lewandowski
(Glenn Research Center Cleveland, Ohio, United States)
J G Myers
(Glenn Research Center Cleveland, Ohio, United States)
R K Prabhu
(Johnson Space Center Houston, Texas, United States)
Date Acquired
January 26, 2023
Subject Category
Aerospace Medicine
Mathematical And Computer Sciences (General)
Meeting Information
Meeting: Human Research Program Investigators’ Workshop (HRP IWS)
Location: Galveston, TX
Country: US
Start Date: February 7, 2023
End Date: February 9, 2023
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 836954.02.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Finite element modeling
Deconditioning
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