Stressed deformable reflector design and pneumatic membrane antenna for cryogenic thermal vacuum chamber testing
Author
Esparza, M.Choi, H.
Kang, H.
d’Aubigny, C.
Pandde, A.
Quach, H.
Chandra, A.
Karfalt, K.
Takashima, Y.
Palisoc, A.
Arenberg, J.W.
Marshall, K.G.
Glynn, C.S.
Godinez, S.M.
Tafoya, M.
Chalifoux, B.
Walker, C.
Kim, D.
Affiliation
Wyant College of Optical Sciences, University of ArizonaLarge Binocular Telescope Observatory, University of Arizona
Lunar and Planetary Laboratory, University of Arizona
Department of Astronomy, University of Arizona
Steward Observatory, University of Arizona
Issue Date
2021Keywords
Bending moment actuatorDeformable antenna
Membrane antenna
Optomechanical design
Radio astronomy
TVAC
Metadata
Show full item recordPublisher
SPIECitation
Esparza, M., Choi, H., Kang, H., d’Aubigny, C., Pandde, A., Quach, H., Chandra, A., Karfalt, K., Takashima, Y., Palisoc, A., Arenberg, J. W., Marshall, K. G., Glynn, C. S., Godinez, S. M., Tafoya, M., Chalifoux, B., Walker, C., & Kim, D. (2021). Stressed deformable reflector design and pneumatic membrane antenna for cryogenic thermal vacuum chamber testing. Proceedings of SPIE - The International Society for Optical Engineering.Rights
Copyright © 2021 SPIE.Collection Information
This item from the UA Faculty Publications collection is made available by the University of Arizona with support from the University of Arizona Libraries. If you have questions, please contact us at repository@u.library.arizona.edu.Abstract
Deformable reflector technology has mainly been used for observations at visible and infrared wavelengths but has yet to be utilized for terahertz wavefront correction. We present an actuator for deformable reflectors that overcomes challenges particular to this wavelength such as a millimeter-scale stroke requirement. Bending moment actuators are used in both the radial and tangential directions to correct low-order wavefront aberrations. Strong and flexible materials such as Delrin are used for the reflector material. Such a deformable antenna can be used to correct wavefronts on future large radio antennae such as the Orbiting Astronomical Satellite for Investigating Stellar Systems (OASIS). This antenna uses a 20-meter thin membrane as its primary radio wave collector. A deformable reflector may be added to this system to allow for looser tolerances on the primary antenna shape and correct for wavefront errors inherent in an inflatable optic. To predict the wavefront errors that may be expected when using this type of thin membrane primary reflector, TVAC (Thermal Vacuum Chamber) test methods are also presented in these proceedings. © 2021 SPIE.Note
Immediate accessISSN
0277-786XISBN
9781510644786Version
Final published versionae974a485f413a2113503eed53cd6c53
10.1117/12.2594403