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MAXI mission for space station and future ASM
Author(s) -
Matsuoka M.,
Sugizaki M.,
Tomida H.,
Torii K.,
Ueno S.,
Kawai N.,
Mihara T.,
Yoshida A.,
Negoro H.,
Shirasaki Y.,
Sakurai I.,
Tsunemi H.,
Miyata E.,
Yamauchi M.
Publication year - 1999
Publication title -
astronomische nachrichten
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.394
H-Index - 63
eISSN - 1521-3994
pISSN - 0004-6337
DOI - 10.1002/1521-3994(199908)320:4/5<275::aid-asna275>3.0.co;2-k
Subject(s) - payload (computing) , sky , physics , detector , angular resolution (graph drawing) , optics , field of view , remote sensing , resolution (logic) , orbit (dynamics) , satellite , dimension (graph theory) , range (aeronautics) , position (finance) , astronomy , aerospace engineering , computer science , geography , engineering , artificial intelligence , mathematics , computer network , finance , combinatorics , network packet , pure mathematics , economics
MAXI (Monitor of All‐sky X‐ray Image) is the first astrophysical payload for Japanese Experiment Module (JEM) to be designed for all sky X‐ray monitoring. MAXI is a slit scanning camera which consists of two kinds of X‐ray detectors; one is one‐dimensional position sensitive proportional counters with total area of about 5000 cm 2 (here we call GSC) and the other is an X‐ray CCD array with total area of about 200 cm 2 (here we call SSC). The GSC subtends a field of view with an angular dimension of 1° × 180°, while the SSC has a field of view of 1° × 90°. Thus, in the course of one station orbit, MAXI can scan almost all sky with a precision of 1 degree and with X‐ray energy range of 0.5‐30 keV. MAXI with a total weight of about 500 kg will be attached to JEM exposed facility (JEM‐EF) in 2004. Furthermore, the future ASM with more sensitive detectors having a wide energy band and with better time response/resolution will follow the MAXI mission.

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