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Design of Mechanisms for Deployable, Optical Instruments: Guidelines for Reducing HysteresisThis paper is intended to facilitate the development of deployable, optical instruments by providing a rational approach for the design, testing, and qualification of high-precision (i.e., low-hysteresis) deployment mechanisms for these instruments. Many of the guidelines included herein come directly from the field of optomechanical engineering, and are, therefore, neither newly developed guidelines, nor are they uniquely applicable to the design of high-precision deployment mechanisms. This paper is to be regarded as a guide to design and not a set of NASA requirements, except as may be defined in formal project specifications. Furthermore, due to the rapid pace of advancement in the field of precision deployment, this paper should be regarded as a preliminary set of guidelines. However, it is expected that this paper, with revisions as experience may indicate to be desirable, might eventually form the basis for a set of uniform design requirements for high-precision deployment mechanisms on future NASA space-based science instruments.
Document ID
20000032952
Document Type
Technical Memorandum (TM)
Authors
Lake, Mark S. (NASA Langley Research Center Hampton, VA United States)
Hachkowski, M. Roman (Raytheon Systems Co. Danbury, CT United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2000
Subject Category
Instrumentation and Photography
Report/Patent Number
NAS 1.15:210089
NASA/TM-2000-210089
L-17970
Funding Number(s)
PROJECT: RTOP 632-64-00-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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