NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Temperature-Controlled Clamping and Releasing MechanismA report describes the development of a mechanism that automatically clamps upon warming and releases upon cooling between temperature limits of approx. =180 K and approx. =293 K. The mechanism satisfied a need specific to a program that involved repeated excursions of a spectrometer between a room-temperature atmospheric environment and a cryogenic vacuum testing environment. The mechanism was also to be utilized in the intended application of the spectrometer, in which the spectrometer would be clamped for protection during launch of a spacecraft and released in the cold of outer space to allow it to assume its nominal configuration for scientific observations. The mechanism is passive in the sense that its operation does not depend on a control system and does not require any power other than that incidental to heating and cooling. The clamping and releasing action is effected by bolt-preloaded stacks of shape-memory-alloy (SMA) cylinders. In designing this mechanism, as in designing other, similar SMA mechanisms, it was necessary to account for the complex interplay among thermal expansion, elastic and inelastic deformation under load, and SMA thermomechanical properties.
Document ID
20110014900
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Rosing, David
(California Inst. of Tech. Pasadena, CA, United States)
Ford, Virginia
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 25, 2013
Publication Date
May 1, 2005
Publication Information
Publication: NASA Tech Briefs, May 2005
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NPO-40541
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available