Paper
21 September 2012 FalconSAT-7: a membrane photon sieve CubeSat solar telescope
Author Affiliations +
Abstract
We are currently constructing FalconSAT-7 for launch in mid-2014. The low-Earth, 3U CubeSat solar telescope incorporates a 0.2m deployable membrane photon sieve with over 2.5 billion holes. The aim of the experiment is to demonstrate diffraction limited imaging of a collapsible, diffractive primary over a narrow bandwidth. As well as being simpler to manufacture and deploy than curved, polished surfaces, the sheets do not have to be optically flat, greatly reducing many engineering issues. As such, the technology is particularly promising as a means to achieve extremely large optical primaries from compact, lightweight packages.
© (2012) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Geoff Andersen, Olha Asmolov, Michael E. Dearborn, and Matthew G. McHarg "FalconSAT-7: a membrane photon sieve CubeSat solar telescope", Proc. SPIE 8442, Space Telescopes and Instrumentation 2012: Optical, Infrared, and Millimeter Wave, 84421C (21 September 2012); https://doi.org/10.1117/12.924250
Lens.org Logo
CITATIONS
Cited by 7 scholarly publications.
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Optics manufacturing

Solar telescopes

Space telescopes

Manufacturing

Polymers

Binary data

Diffraction

RELATED CONTENT

FalconSAT-7: a membrane space telescope
Proceedings of SPIE (August 28 2014)
FalconSAT-7: a membrane space telescope
Proceedings of SPIE (June 03 2014)
FalconSAT-7: a membrane space solar telescope
Proceedings of SPIE (July 29 2016)
Membrane photon sieve telescope
Proceedings of SPIE (May 24 2012)
Membrane photon sieve telescope
Proceedings of SPIE (September 21 2011)
Net-shape polymer mirrors
Proceedings of SPIE (February 01 2002)
Lightweighted mirrors for space telescopes
Proceedings of SPIE (June 01 1994)

Back to Top