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In-Situ Focusing Inside a Thermal Vacuum ChamberTraditionally, infrared (IR) space instruments have been focused by iterating with a number of different thickness shim rings in a thermal vacuum chamber until the focus meets requirements. This has required a number of thermal cycles that are very expensive as they tie up many integration and test (I&T)/ environmental technicians/engi neers work ing three shifts for weeks. Rather than creating a test shim for each iteration, this innovation replaces the test shim and can focus the instrument while in the thermal vacuum chamber. The focus tool consists of three small, piezo-actuated motors that drive two sets of mechanical interface flanges between the instrument optics and the focal- plane assembly, and three optical-displacement metrology sensors that can be read from outside the thermal vacuum chamber. The motors are used to drive the focal planes to different focal distances and acquire images, from which it is possible to determine the best focus. At the best focus position, the three optical displacement metrology sensors are used to determine the shim thickness needed. After the instrument leaves the thermal vacuum chamber, the focus tool is replaced with the precision-ground shim ring. The focus tool consists of two sets of collars, one that mounts to the backside of the interface flange of the instrument optics, and one that mounts to the backside of the interface flange of the focal plane modules. The collars on the instrument optics side have the three small piezo-actuated motors and the three optical displacement metrology systems. Before the instrument is focused, there is no shim ring in place and, therefore, no fasteners holding the focal plane modules to the cameras. Two focus tooling collars are held together by three strong springs. The Orbiting Carbon Observatory (OCO) mission spectrometer was focused this way (see figure). The motor described here had to be moved five times to reach an acceptable focus, all during the same thermal cycle, which was verified using pupil slicing techniques. A focus accuracy of .20.100 microns was achieved.
Document ID
20100001373
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Liebe, Carl Christian
(California Inst. of Tech. Pasadena, CA, United States)
Hannah, Brett
(California Inst. of Tech. Pasadena, CA, United States)
Bartman, Randall
(California Inst. of Tech. Pasadena, CA, United States)
Radulescu, Costin
(California Inst. of Tech. Pasadena, CA, United States)
Rud, Mayer
(California Inst. of Tech. Pasadena, CA, United States)
Sarkissian, Edwin
(California Inst. of Tech. Pasadena, CA, United States)
Ho, Timothy
(California Inst. of Tech. Pasadena, CA, United States)
Pollock, Randy
(Hamilton Sundstrand United States)
Esposito, Joseph
(Hamilton Sundstrand United States)
Sutin, Brian
(Hamilton Sundstrand United States)
Haring, Robert
(Hamilton Sundstrand United States)
Gonzalez, Juan
(Gonzalez (Juan) United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2010
Publication Information
Publication: NASA Tech Briefs, January 2010
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NPO-45749
Distribution Limits
Public
Copyright
Public Use Permitted.
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