Hannah Gulick, Jessica R. Lu, Aryan Sood, Steven V. W. Beckwith, Joshua S. Bloom, Kodi Rider, Dan Werthimer, Wei Liu, Guy Nir, Harrison Lee, Jeremy McCauley
{"title":"CuRIOS-ED: The Technology Demonstrator for the CubeSats for Rapid Infrared and Optical Surveys Mission","authors":"Hannah Gulick, Jessica R. Lu, Aryan Sood, Steven V. W. Beckwith, Joshua S. Bloom, Kodi Rider, Dan Werthimer, Wei Liu, Guy Nir, Harrison Lee, Jeremy McCauley","doi":"arxiv-2409.11471","DOIUrl":null,"url":null,"abstract":"The rise of time-domain astronomy including electromagnetic counterparts to\ngravitational waves, gravitational microlensing, explosive phenomena, and even\nastrometry with Gaia, are showing the power and need for surveys with\nhigh-cadence, large area, and long time baselines to study the transient\nuniverse. A constellation of SmallSats or CubeSats providing wide,\ninstantaneous sky coverage down to 21 Vega mag at optical wavelengths would be\nideal for addressing this need. We are assembling CuRIOS-ED (CubeSats for Rapid\nInfrared and Optical Survey--Exploration Demo), an optical telescope payload\nwhich will act as a technology demonstrator for a larger constellation of\nseveral hundred 16U CubeSats known as CuRIOS. In preparation for CuRIOS,\nCuRIOS-ED will launch in late 2025 as part of the 12U Starspec InspireSat MVP\npayload. CuRIOS-ED will be used to demonstrate the StarSpec ADCS pointing\ncapabilities to <1\" and to space-qualify a commercial camera package for use on\nthe full CuRIOS payload. The CuRIOS-ED camera system will utilize a Sony IMX455\nCMOS detector delivered in an off-the-shelf Atik apx60 package which we\nmodified to be compatible with operations in vacuum as well as the CubeSat form\nfactor, power, and thermal constraints. By qualifying this commercial camera\nsolution, the cost of each CuRIOS satellite will be greatly decreased (~100x)\nwhen compared with current space-qualified cameras with IMX455 detectors. We\ndiscuss the CuRIOS-ED mission design with an emphasis on the disassembly,\nrepackaging, and testing of the Atik apx60 for space-based missions.\nCharacterization of the apx60's read noise, dark current, patterned noise, and\nthermal behavior are reported for a range of temperatures (-35 C to 40 C) and\nexposure times (0.001s to 30 s). Additionally, we comment on preliminary\nenvironmental testing results from a successful thermal vacuum test.","PeriodicalId":501163,"journal":{"name":"arXiv - PHYS - Instrumentation and Methods for Astrophysics","volume":"29 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"arXiv - PHYS - Instrumentation and Methods for Astrophysics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/arxiv-2409.11471","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
The rise of time-domain astronomy including electromagnetic counterparts to
gravitational waves, gravitational microlensing, explosive phenomena, and even
astrometry with Gaia, are showing the power and need for surveys with
high-cadence, large area, and long time baselines to study the transient
universe. A constellation of SmallSats or CubeSats providing wide,
instantaneous sky coverage down to 21 Vega mag at optical wavelengths would be
ideal for addressing this need. We are assembling CuRIOS-ED (CubeSats for Rapid
Infrared and Optical Survey--Exploration Demo), an optical telescope payload
which will act as a technology demonstrator for a larger constellation of
several hundred 16U CubeSats known as CuRIOS. In preparation for CuRIOS,
CuRIOS-ED will launch in late 2025 as part of the 12U Starspec InspireSat MVP
payload. CuRIOS-ED will be used to demonstrate the StarSpec ADCS pointing
capabilities to <1" and to space-qualify a commercial camera package for use on
the full CuRIOS payload. The CuRIOS-ED camera system will utilize a Sony IMX455
CMOS detector delivered in an off-the-shelf Atik apx60 package which we
modified to be compatible with operations in vacuum as well as the CubeSat form
factor, power, and thermal constraints. By qualifying this commercial camera
solution, the cost of each CuRIOS satellite will be greatly decreased (~100x)
when compared with current space-qualified cameras with IMX455 detectors. We
discuss the CuRIOS-ED mission design with an emphasis on the disassembly,
repackaging, and testing of the Atik apx60 for space-based missions.
Characterization of the apx60's read noise, dark current, patterned noise, and
thermal behavior are reported for a range of temperatures (-35 C to 40 C) and
exposure times (0.001s to 30 s). Additionally, we comment on preliminary
environmental testing results from a successful thermal vacuum test.