Loading…

Optical Disk Recorder (ODR) for Satellite Use

An earth-observing satellite flies at an altitude of 800 km. The data acquired while the satellite flies at the opposite side of the earth from a telemetry station has to be stored in the satellite because it is difficult to establish a communication channel between the telemetry station and the sat...

Full description

Saved in:
Bibliographic Details
Published in:Japanese Journal of Applied Physics 2005-05, Vol.44 (5S), p.3432
Main Authors: Tanaka, Kunimaro, Itoh, Osamu, Iwai, Hitoshi, Kasuya, Masahiro
Format: Article
Language:English
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by
cites
container_end_page
container_issue 5S
container_start_page 3432
container_title Japanese Journal of Applied Physics
container_volume 44
creator Tanaka, Kunimaro
Itoh, Osamu
Iwai, Hitoshi
Kasuya, Masahiro
description An earth-observing satellite flies at an altitude of 800 km. The data acquired while the satellite flies at the opposite side of the earth from a telemetry station has to be stored in the satellite because it is difficult to establish a communication channel between the telemetry station and the satellite. The use of the first optical disk recorder (ODR) in space has been planned [H. Anegawa, T. Fukuda, S. Yamamoto, D. Maeusli and M. Kasuya: Proc. Int. Symp. Optical Memory '91 , (1991) p. 115; H. Anegawa, K. Tanaka and N. Tsuya: Proc. Optical Data Storage '92 p. 1 MD4 (1992)]. To make the optical disk drive work in space, the following measure was taken. The large acceleration during launching was solved using the launch lock mechanism. The temperature control mechanism was used to cope with a wide temperature change. Optical components were carefully selected for cosmic ray. ADEOS-II at which the ODR was installed was launched on December 14, 2002. The ODR had worked correctly for about ten months until the solar cell of the satellite stopped functioning. It was proved that the optical disk drive can work in space when an appropriate measure is taken.
doi_str_mv 10.1143/JJAP.44.3432
format article
fullrecord <record><control><sourceid>crossref</sourceid><recordid>TN_cdi_crossref_primary_10_1143_JJAP_44_3432</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>10_1143_JJAP_44_3432</sourcerecordid><originalsourceid>FETCH-LOGICAL-c340t-3a0a7c9876fb0d9311b4b5b56055bd1acd2b6207bcd3d1f0d353ceb387cf37973</originalsourceid><addsrcrecordid>eNotz81KAzEUhuEgCo7VnReQpYIZk5yTSWdZWv9KYaTadcgvjI5MSWbj3eugq49388FDyLXgtRAI99vt6rVGrAFBnpBKAGqGvFGnpOJcCoatlOfkopSP32wUioqw7jj13g5005dPuo9-zCFmetNt9rc0jZm-2SkOQz9FeijxkpwlO5R49b8Lcnh8eF8_s1339LJe7ZgH5BMDy6327VI3yfHQghAOnXKq4Uq5IKwP0jWSa-cDBJF4AAU-Olhqn0C3Ghbk7u_X57GUHJM55v7L5m8juJmpZqYaRDNT4QdvC0Su</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>Optical Disk Recorder (ODR) for Satellite Use</title><source>IOPscience journals</source><source>Institute of Physics:Jisc Collections:IOP Publishing Read and Publish 2024-2025 (Reading List)</source><creator>Tanaka, Kunimaro ; Itoh, Osamu ; Iwai, Hitoshi ; Kasuya, Masahiro</creator><creatorcontrib>Tanaka, Kunimaro ; Itoh, Osamu ; Iwai, Hitoshi ; Kasuya, Masahiro</creatorcontrib><description>An earth-observing satellite flies at an altitude of 800 km. The data acquired while the satellite flies at the opposite side of the earth from a telemetry station has to be stored in the satellite because it is difficult to establish a communication channel between the telemetry station and the satellite. The use of the first optical disk recorder (ODR) in space has been planned [H. Anegawa, T. Fukuda, S. Yamamoto, D. Maeusli and M. Kasuya: Proc. Int. Symp. Optical Memory '91 , (1991) p. 115; H. Anegawa, K. Tanaka and N. Tsuya: Proc. Optical Data Storage '92 p. 1 MD4 (1992)]. To make the optical disk drive work in space, the following measure was taken. The large acceleration during launching was solved using the launch lock mechanism. The temperature control mechanism was used to cope with a wide temperature change. Optical components were carefully selected for cosmic ray. ADEOS-II at which the ODR was installed was launched on December 14, 2002. The ODR had worked correctly for about ten months until the solar cell of the satellite stopped functioning. It was proved that the optical disk drive can work in space when an appropriate measure is taken.</description><identifier>ISSN: 0021-4922</identifier><identifier>EISSN: 1347-4065</identifier><identifier>DOI: 10.1143/JJAP.44.3432</identifier><language>eng</language><ispartof>Japanese Journal of Applied Physics, 2005-05, Vol.44 (5S), p.3432</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,777,781,27905,27906</link.rule.ids></links><search><creatorcontrib>Tanaka, Kunimaro</creatorcontrib><creatorcontrib>Itoh, Osamu</creatorcontrib><creatorcontrib>Iwai, Hitoshi</creatorcontrib><creatorcontrib>Kasuya, Masahiro</creatorcontrib><title>Optical Disk Recorder (ODR) for Satellite Use</title><title>Japanese Journal of Applied Physics</title><description>An earth-observing satellite flies at an altitude of 800 km. The data acquired while the satellite flies at the opposite side of the earth from a telemetry station has to be stored in the satellite because it is difficult to establish a communication channel between the telemetry station and the satellite. The use of the first optical disk recorder (ODR) in space has been planned [H. Anegawa, T. Fukuda, S. Yamamoto, D. Maeusli and M. Kasuya: Proc. Int. Symp. Optical Memory '91 , (1991) p. 115; H. Anegawa, K. Tanaka and N. Tsuya: Proc. Optical Data Storage '92 p. 1 MD4 (1992)]. To make the optical disk drive work in space, the following measure was taken. The large acceleration during launching was solved using the launch lock mechanism. The temperature control mechanism was used to cope with a wide temperature change. Optical components were carefully selected for cosmic ray. ADEOS-II at which the ODR was installed was launched on December 14, 2002. The ODR had worked correctly for about ten months until the solar cell of the satellite stopped functioning. It was proved that the optical disk drive can work in space when an appropriate measure is taken.</description><issn>0021-4922</issn><issn>1347-4065</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2005</creationdate><recordtype>article</recordtype><recordid>eNotz81KAzEUhuEgCo7VnReQpYIZk5yTSWdZWv9KYaTadcgvjI5MSWbj3eugq49388FDyLXgtRAI99vt6rVGrAFBnpBKAGqGvFGnpOJcCoatlOfkopSP32wUioqw7jj13g5005dPuo9-zCFmetNt9rc0jZm-2SkOQz9FeijxkpwlO5R49b8Lcnh8eF8_s1339LJe7ZgH5BMDy6327VI3yfHQghAOnXKq4Uq5IKwP0jWSa-cDBJF4AAU-Olhqn0C3Ghbk7u_X57GUHJM55v7L5m8juJmpZqYaRDNT4QdvC0Su</recordid><startdate>20050501</startdate><enddate>20050501</enddate><creator>Tanaka, Kunimaro</creator><creator>Itoh, Osamu</creator><creator>Iwai, Hitoshi</creator><creator>Kasuya, Masahiro</creator><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20050501</creationdate><title>Optical Disk Recorder (ODR) for Satellite Use</title><author>Tanaka, Kunimaro ; Itoh, Osamu ; Iwai, Hitoshi ; Kasuya, Masahiro</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c340t-3a0a7c9876fb0d9311b4b5b56055bd1acd2b6207bcd3d1f0d353ceb387cf37973</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2005</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Tanaka, Kunimaro</creatorcontrib><creatorcontrib>Itoh, Osamu</creatorcontrib><creatorcontrib>Iwai, Hitoshi</creatorcontrib><creatorcontrib>Kasuya, Masahiro</creatorcontrib><collection>CrossRef</collection><jtitle>Japanese Journal of Applied Physics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Tanaka, Kunimaro</au><au>Itoh, Osamu</au><au>Iwai, Hitoshi</au><au>Kasuya, Masahiro</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Optical Disk Recorder (ODR) for Satellite Use</atitle><jtitle>Japanese Journal of Applied Physics</jtitle><date>2005-05-01</date><risdate>2005</risdate><volume>44</volume><issue>5S</issue><spage>3432</spage><pages>3432-</pages><issn>0021-4922</issn><eissn>1347-4065</eissn><abstract>An earth-observing satellite flies at an altitude of 800 km. The data acquired while the satellite flies at the opposite side of the earth from a telemetry station has to be stored in the satellite because it is difficult to establish a communication channel between the telemetry station and the satellite. The use of the first optical disk recorder (ODR) in space has been planned [H. Anegawa, T. Fukuda, S. Yamamoto, D. Maeusli and M. Kasuya: Proc. Int. Symp. Optical Memory '91 , (1991) p. 115; H. Anegawa, K. Tanaka and N. Tsuya: Proc. Optical Data Storage '92 p. 1 MD4 (1992)]. To make the optical disk drive work in space, the following measure was taken. The large acceleration during launching was solved using the launch lock mechanism. The temperature control mechanism was used to cope with a wide temperature change. Optical components were carefully selected for cosmic ray. ADEOS-II at which the ODR was installed was launched on December 14, 2002. The ODR had worked correctly for about ten months until the solar cell of the satellite stopped functioning. It was proved that the optical disk drive can work in space when an appropriate measure is taken.</abstract><doi>10.1143/JJAP.44.3432</doi></addata></record>
fulltext fulltext
identifier ISSN: 0021-4922
ispartof Japanese Journal of Applied Physics, 2005-05, Vol.44 (5S), p.3432
issn 0021-4922
1347-4065
language eng
recordid cdi_crossref_primary_10_1143_JJAP_44_3432
source IOPscience journals; Institute of Physics:Jisc Collections:IOP Publishing Read and Publish 2024-2025 (Reading List)
title Optical Disk Recorder (ODR) for Satellite Use
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-19T20%3A08%3A43IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-crossref&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Optical%20Disk%20Recorder%20(ODR)%20for%20Satellite%20Use&rft.jtitle=Japanese%20Journal%20of%20Applied%20Physics&rft.au=Tanaka,%20Kunimaro&rft.date=2005-05-01&rft.volume=44&rft.issue=5S&rft.spage=3432&rft.pages=3432-&rft.issn=0021-4922&rft.eissn=1347-4065&rft_id=info:doi/10.1143/JJAP.44.3432&rft_dat=%3Ccrossref%3E10_1143_JJAP_44_3432%3C/crossref%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c340t-3a0a7c9876fb0d9311b4b5b56055bd1acd2b6207bcd3d1f0d353ceb387cf37973%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true