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Comparison of Anthropomorphic Test Device and Human Volunteer Responses in Simulated Landing Impact Tests of U.S. Space VehiclesUnited States (U.S.) crewed vehicles are being designed to support the National Aeronautics and Space Administration’s (NASA’s) human spaceflight programs. Vehicles must be designed to meet NASA’s occupant protection requirements including landing injury assessment with anthropomorphic test devices (ATDs) and analytical models. However, these tools are limited in capturing all injuries that might occur during spacecraft landings. A NASA study of injuries during Soyuz vehicle landings has shown that analytical models are underpredicting occupant injury. Because of the inherent limitations with our analytical tools, human volunteer impact testing was employed to assess flight-like landing conditions of U.S. crewed vehicles. A total of 84 human volunteer tests in 11 different test orientations and g-levels were completed as part of this effort in collaboration with the Air Force Research Laboratory (AFRL) at Wright-Patterson Air Force Base and U.S. vehicle development companies. Human subjects were tested at various realistic landing loads and in the highest fidelity seat and suit components that were available at the time of testing for two U.S. vehicles. Matched-pair ATD tests in the same test conditions were also conducted with small female and midsized male Hybrid III ATDs. ATDs were fully instrumented. Head accelerations and subjective responses were recorded for human subjects. In some cases, chest accelerations were captured. Responses of the ATDs and humans in matched-pair tests were compared. No ATD tests showed evidence for risk of injury based on NASA occupant protection requirements. Human subjects reported 17 cases of discomfort or pain, and 1 human subject was diagnosed with a minor injury that was not evident in the ATD tests. These results provide evidence that ATDs do not capture all potential injury risks, namely lower severity injuries, discomfort, pain, and fit issues. Overall, human testing is beneficial to understanding the true risk of injury to crewmembers during Earth landings.
Document ID
20240005349
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Teresa M Reiber
(KBR (United States) Houston, Texas, United States)
Preston C Greenhalgh
(KBR (United States) Houston, Texas, United States)
Keegan M Yates
(KBR (United States) Houston, Texas, United States)
Rachel L Thompson
(KBR (United States) Houston, Texas, United States)
Aaron M Drake
(KBR (United States) Houston, Texas, United States)
Nathaniel Newby
(KBR (United States) Houston, Texas, United States)
Jeffrey T Somers ORCID
(Johnson Space Center Houston, United States)
Dustin M Gohmert
(Johnson Space Center Houston, United States)
Jeffrey D Suhey
(Johnson Space Center Houston, United States)
Chris E Perry
(United States Air Force Research Laboratory Wright-Patterson AFB, United States)
John R Buhrman
(United States Air Force Research Laboratory Wright-Patterson AFB, United States)
Mark A Baldwin
(Lockheed Martin (United States) Bethesda, United States)
Cynthia H Null
(Ames Research Center Mountain View, United States)
Date Acquired
April 29, 2024
Publication Date
July 21, 2024
Publication Information
Issue Publication Date: July 8, 2024
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
ICES-2024-345
Meeting Information
Meeting: 53rd International Conference on Environmental Systems (ICES)
Location: Louisville, KY
Country: US
Start Date: July 21, 2024
End Date: July 25, 2024
Sponsors: International Conference on Environmental Systems
Funding Number(s)
WBS: 10449.2.03.02.28.1341
CONTRACT_GRANT: NNJ15HK11B
CONTRACT_GRANT: NNJ06TA25C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
External Peer Committee
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