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Partial gravity simulation using a pneumatic actuator with closed loop mechanical amplificationTo support future manned missions to the surface of the Moon and Mars or missions requiring manipulation of payloads and locomotion in space, a training device is required to simulate the conditions of both partial and microgravity as compared to the gravity on Earth. The focus of this paper is to present the development, construction, and testing of a partial gravity simulator which uses a pneumatic actuator with closed loop mechanical amplification. Results of the testing show that this type of simulator maintains a constant partial gravity simulation with a variation of the simulated body force between 2.2 percent and 10 percent, depending on the type of locomotion inputs. The data collected using the simulator show that mean stride frequencies at running speeds at lunar and Martian gravity levels are 12 percent less than those at Earth gravity. The data also show that foot/ground reaction forces at lunar and Martian gravity are, respectively, 62 percent and 51 percent less than those on Earth.
Document ID
19940029889
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ray, David M.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
NASA-TM-104798
NAS 1.15:104798
S-772
Report Number: NASA-TM-104798
Report Number: NAS 1.15:104798
Report Number: S-772
Accession Number
94N34395
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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