Earth Observing Systems XXII 2017
DOI: 10.1117/12.2272839
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Design and development of the CubeSat Infrared Atmospheric Sounder (CIRAS)

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Cited by 9 publications
(7 citation statements)
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“…CRTM has been widely used in simulating synthetic observations (Boukabara et al 2018). The CRTM team (Tong Zhu and Sid Boukabara, personal communication, 2017) have developed and delivered the optical depth in pressure space coefficients required to use CRTM for both CIRAS and MicroMAS-2 based on the spectral response function (SRF) provided by JPL (Pagano et al 2017) and MIT/LL (Blackwell et al 2018). CRTM does not include nonlocal thermodynamic equilibrium (NLTE) effects in radiance simulation around the 4.3 μm CO 2 absorption band, which may contribute brightness temperature (T b ) error of about 1-1.5 K for those CIRAS channels.…”
Section: Synthetic Observation Simulationmentioning
confidence: 99%
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“…CRTM has been widely used in simulating synthetic observations (Boukabara et al 2018). The CRTM team (Tong Zhu and Sid Boukabara, personal communication, 2017) have developed and delivered the optical depth in pressure space coefficients required to use CRTM for both CIRAS and MicroMAS-2 based on the spectral response function (SRF) provided by JPL (Pagano et al 2017) and MIT/LL (Blackwell et al 2018). CRTM does not include nonlocal thermodynamic equilibrium (NLTE) effects in radiance simulation around the 4.3 μm CO 2 absorption band, which may contribute brightness temperature (T b ) error of about 1-1.5 K for those CIRAS channels.…”
Section: Synthetic Observation Simulationmentioning
confidence: 99%
“…Second, from its polar sun-synchronous orbit, the 6U CubeSat Infrared Atmospheric Sounder (CIRAS), an AIRSlike hyperspectral IR sounder, will measure the upwelling IR radiation of the Earth and its atmosphere in 625 shortwave IR (SWIR) spectral channels (1949-2451 cm −1 , or 4.08--5.13 μm, including the 4.3 μm CO 2 absorption band) (Pagano et al 2017). CIRAS has a spectral resolution of 1.2-2.0 cm −1 and a Noise Equivalent differential Temperature (NEdT) of 0.1-0.4 K (increasing with frequency) at 250 K. The CIRAS horizontal resolution of 13.5 km covers a swath 1100 km wide.…”
Section: Introductionmentioning
confidence: 99%
“…The CIRAS is currently designed for a 6U or 12U CubeSat developed by Blue Canyon Technologies, but can be easily accommodated by a variety of small spacecraft. A description of the CIRAS instrument concept, enabling technologies, and expected performance has been provided in prior works 5,6 .…”
Section: Ciras Instrumentmentioning
confidence: 99%
“…On one hand, technological advances result in sensor designs with higher spatial, temporal, and spectral resolution. In addition, miniaturization permits deployment on less expensive SmallSat and CubeSat platforms [e.g., CIRAS described by Pagano et al (2017) and MicroMAS-2 described by Blackwell et al (2019)]. As a result, we are now seeing the emergence of commercial space-based data from flotillas of small satellites being marketed by multiple industry players.…”
Section: Satellite Remote Sensing and Nwpmentioning
confidence: 99%