NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Proposal for an astronaut mass measurement device for the Space ShuttleFor medical reasons, astronauts in space need to have their mass measured. Currently, this measurement is performed using a mass-spring system. The current system is large, inaccurate, and uncomfortable for the astronauts. NASA is looking for new, different, and preferably better ways to perform this measurement process. After careful analysis our design team decided on a linear acceleration process. Within the process, four possible concept variants are put forth. Among these four variants, one is suggested over the others. The variant suggested is that of a motor-winch system to linearly accelerate the astronaut. From acceleration and force measurements of the process combined Newton's second law, the mass of an astronaut can be calculated.
Document ID
19950008440
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Beyer, Neil
(Universities Space Research Association Columbia, MD, United States)
Lomme, Jon
(Universities Space Research Association Columbia, MD, United States)
Mccollough, Holly
(Universities Space Research Association Columbia, MD, United States)
Price, Bradford
(Universities Space Research Association Columbia, MD, United States)
Weber, Heidi
(Universities Space Research Association Columbia, MD, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1994
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NASA-CR-197198
NAS 1.26:197198
Report Number: NASA-CR-197198
Report Number: NAS 1.26:197198
Accession Number
95N14854
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available