Matsuhara, Hideo, Kawada, Mitsunobu, Matsumoto, Toshio, Matsuura, Shuji, Tanaka, Masahiro, Bock, James J., Hristov, Viktor V., Lange, Andrew E., Mauskopf, Philip Daniel ![]() |
Abstract
We give a detailed description of the design and flight performance of an instrument onboard the S-520-15 rocket of the Institute of Space and Astronautical Science. The isntrument, consisting of a near-infrared spectrometer and a far-infrared photometer at the focus of a 10 cm liquid-helium cooled telescope, was designed to observe both the brightness and distribution of diffuse emission with high sensitivity. The rocket was successfully launched and the instrument observed near-infrared and far-infrared continuum emission, as well as (C II) 157.7 micrometer line emission from regions at high Galactic latitude. We also give a brief description of the design and performance of an onboard attitude control system.
Item Type: | Article |
---|---|
Date Type: | Publication |
Status: | Published |
Schools: | Physics and Astronomy |
Subjects: | Q Science > QB Astronomy |
Uncontrolled Keywords: | Design Analysis, Infrared Photometry, Infrared Spectrometers, Infrared Telescopes, Rocket-Borne instruments, astronomical photometry, carbon, far infrared R radiation, galactic radiation, line spectra, near infrared radiation |
Publisher: | Astronomical Society of Japan |
ISSN: | 0004-6264 |
Last Modified: | 28 Oct 2022 08:28 |
URI: | https://orca.cardiff.ac.uk/id/eprint/70915 |
Citation Data
Actions (repository staff only)
![]() |
Edit Item |