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Mechanism Design Principle for Optical-Precision, Deployable InstrumentsThe present paper is intended to be a guide for the design of 'microdynamically quiet' deployment mechanisms for optical-precision structures, such as deployable telescope mirrors and optical benches. Many of the guidelines included herein come directly from the field of optomechanical engineering, and are neither newly developed guidelines nor are they uniquely applicable to high-precision deployment mechanisms. However, the application of these guidelines to the design of deployment mechanisms is a rather new practice, so efforts are made herein to illustrate the process through the discussion of specific examples. The present paper summarizes a more extensive set of design guidelines for optical-precision mechanisms that are under development.
Document ID
20040086761
Acquisition Source
Langley Research Center
Document Type
Conference Paper
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
January 1, 2000
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA Paper 2000-1409
Report Number: AIAA Paper 2000-1409
Meeting Information
Meeting: 41st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Atlanta, GA
Country: United States
Start Date: April 3, 2000
End Date: April 6, 2000
Sponsors: American Helicopter Society, Inc., American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Society of Civil Engineers, American Society for Composites
Distribution Limits
Public
Copyright
Public Use Permitted.
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