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Reach performance while wearing the Space Shuttle launch and entry suit during exposure to launch accelerationsA crew of four veteran astronaut/pilots were subjected to sustained linear accelerations of up to 3G(x) in order to quantify crew reach performance while wearing the currently used Launch and Entry Suit (LES). Photogrammetric techniques were used to quantify magnitudes of reach in any direction while subjects rode a centrifuge. Subjects exhibited small changes of reach capability in the +x (forward) direction which ranged from an improvement of 2.04 cm to a decrease of 14.4 cm while reach performance in the +z (overhead) direction was improved in three of four subjects, indicating that any task which could be accomplished under exposure to 1G(x) could definitely be done at 3G(x). The data from this experiment demonstrated that Shuttle crews in training can expect to maintain all of the overhead reach capability evident in good simulator runs and suffer only moderate degradation in the forward reach performance during the launch phase of an actual Shuttle mission.
Document ID
19900062335
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bagian, James P.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Greenisen, M. C.
(NASA Johnson Space Center Houston, TX, United States)
Schafer, L. E.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Probe, J. D.
(Lockheed Engineering and Sciences Co. Houston, TX, United States)
Krutz, Robert W., Jr.
(Krug International, San Antonio; USAF, School of Aerospace Medicine, Brooks AFB TX, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Man/System Technology And Life Support
Report/Patent Number
SAE PAPER 901357
Accession Number
90A49390
Distribution Limits
Public
Copyright
Other

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