Scipediacontent: Scipediacontent moved page Draft Content 564675240 to Okada et al 2016a

2020-10-14T12:52:24Z

Scipediacontent moved page Draft Content 564675240 to Okada et al 2016a

Scipediacontent: Created page with " == Abstract == The thermal infrared imager TIR onboard Hayabusa2 has been developed to investigate thermo-physical properties of C-type, near-Earth asteroid 162173 Ryugu. TI..."

2020-10-14T12:52:22Z

Created page with " == Abstract == The thermal infrared imager TIR onboard Hayabusa2 has been developed to investigate thermo-physical properties of C-type, near-Earth asteroid 162173 Ryugu. TI..."

New page

== Abstract ==

The thermal infrared imager TIR onboard Hayabusa2 has been developed to investigate thermo-physical properties of C-type, near-Earth asteroid 162173 Ryugu. TIR is one of the remote science instruments on Hayabusa2 designed to understand the nature of a volatile-rich solar system small body, but it also has significant mission objectives to provide information on surface physical properties and conditions for sampling site selection as well as the assessment of safe landing operations. TIR is based on a two-dimensional uncooled micro-bolometer array inherited from the Longwave Infrared Camera LIR on Akatsuki (Fukuhara et al., 2011). TIR takes images of thermal infrared emission in 8 to 12 ?m with a field of view of \(16 \times 12^{\circ}\) and a spatial resolution of \(0.05^{\circ}\) per pixel. TIR covers the temperature range from 150 to 460 K, including the well calibrated range from 230 to 420 K. Temperature accuracy is within 2 K or better for summed images, and the relative accuracy or noise equivalent temperature difference (NETD) at each of pixels is 0.4 K or lower for the well-calibrated temperature range. TIR takes a couple of images with shutter open and closed, the corresponding dark frame, and provides a true thermal image by dark frame subtraction. Data processing involves summation of multiple images, image processing including the StarPixel compression (Hihara et al., 2014), and transfer to the data recorder in the spacecraft digital electronics (DE). We report the scientific and mission objectives of TIR, the requirements and constraints for the instrument specifications, the designed instrumentation and the pre-flight and in-flight performances of TIR, as well as its observation plan during the Hayabusa2 mission.

Document type: Part of book or chapter of book

== Full document ==
<pdf>Media:Draft_Content_564675240-beopen650-1274-document.pdf</pdf>

== Original document ==

The different versions of the original document can be found in:

* [http://dspace.stir.ac.uk/bitstream/1893/26994/1/Okada-etal-SpaceScienceReviews-2017.pdf http://dspace.stir.ac.uk/bitstream/1893/26994/1/Okada-etal-SpaceScienceReviews-2017.pdf] under the license cc-by

DOIS: 10.1007/s11214-016-0286-8 10.1007/978-94-024-1538-4_15

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Okada et al 2016a - Revision history

Scipediacontent: Scipediacontent moved page Draft Content 564675240 to Okada et al 2016a

Scipediacontent: Created page with " == Abstract == The thermal infrared imager TIR onboard Hayabusa2 has been developed to investigate thermo-physical properties of C-type, near-Earth asteroid 162173 Ryugu. TI..."