About: TeikyoSat-3

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TeikyoSat-3 was a technology demonstrator and microbiology microsatellite intended to research the slime mold life cycle in space. Specifically, the effects of ionizing radiation (20-30 Gy/year) are or special concern. The primary mission is expected to be finished in 10–20 days with completion of first life cycle of slime mold in space, but mission can be extended to study evolutionary adaptations for a maximum of 1 year. Also, a novel thermal control system capable of keeping a stable (10 °C to 28 °C) temperature in small (20 kg) microsatellite bus is being tested. The satellite is made in Teikyo University (Japan) and has a size of 320x320x370mm. The microsatellite microbiology experimental platform is intended to address issues with cost and uncertain future of experiments based on Int

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rdf:type	Thing schema:Event dul:Event societal event wikidata:Q1656682 wikidata:Q2133344 yago:Artifact100021939 yago:Conveyance103100490 yago:Craft103125870 yago:Equipment103294048 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 yago:WikicatJapaneseSatellitesAndSpaceProbes aircraft event space mission yago:Satellite104137444 yago:Spacecraft104264914 yago:Vehicle104524313 yago:Whole100003553
rdfs:label	TeikyoSat-3 (in) TeikyoSat-3 (en)
rdfs:comment	TeikyoSat-3 adalah demonstrator teknologi dan mikrobiologi marbology dimaksudkan untuk penelitian siklus hidup jamur lendir pada spesies sacromontarism. TeikyoSat-3 juga mengirimkan telemetri yang uncoded di 473,45 MHz, dan setiap operator radio amatir dipersilahkan untuk berbagi data downlink. (in) TeikyoSat-3 was a technology demonstrator and microbiology microsatellite intended to research the slime mold life cycle in space. Specifically, the effects of ionizing radiation (20-30 Gy/year) are or special concern. The primary mission is expected to be finished in 10–20 days with completion of first life cycle of slime mold in space, but mission can be extended to study evolutionary adaptations for a maximum of 1 year. Also, a novel thermal control system capable of keeping a stable (10 °C to 28 °C) temperature in small (20 kg) microsatellite bus is being tested. The satellite is made in Teikyo University (Japan) and has a size of 320x320x370mm. The microsatellite microbiology experimental platform is intended to address issues with cost and uncertain future of experiments based on Int (en)
foaf:name	TeikyoSat-3 (en)
foaf:homepage	http://www.teikyo-u.ac.jp/affiliate/teikyosat/summary.html
name	TeikyoSat-3 (en)
dcterms:subject	Spacecraft which reentered in 2014 2014 in Japan Satellites of Japan Spacecraft launched in 2014
Wikipage page ID	42470274 (xsd:integer)
Wikipage revision ID	1053178899 (xsd:integer)
Link from a Wikipage to another Wikipage	Slime mold Geocentric orbit Mitsubishi Heavy Industries Spacecraft which reentered in 2014 2014 in Japan H-IIA International Space Station Ionizing radiation Tanegashima Space Center Teikyo University Satellites of Japan Spacecraft launched in 2014 Yoshinobu Launch Complex Low Earth orbit
Link from a Wikipage to an external page	http://club.uccl.teikyo-u.ac.jp/~space_system_society/teikyosat-3.html http://www.teikyo-u.ac.jp/affiliate/teikyosat/summary.html http://space.skyrocket.de/doc_sdat/teikyosat-3.htm
sameAs	TeikyoSat-3 TeikyoSat-3 TeikyoSat-3 TeikyoSat-3
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_spaceflight dbt:Portal dbt:Refimprove dbt:Reflist dbt:Use_American_English dbt:Use_dmy_dates dbt:End-date dbt:Start-date dbt:Orbital_launches_in_2014 dbt:Japan-spacecraft-stub
apsis	gee (en)
COSPAR ID	2014 (xsd:integer)
decay date	2014-10-25 (xsd:date)
launch contractor	Mitsubishi Heavy Industries
launch date	0001-02-27 (xsd:gMonthDay)
launch rocket	H-IIA 202 (en)
launch site	Tanegashima Space Center Yoshinobu Launch Complex
manufacturer	Teikyo University
mission type	Technology (en)
operator	Teikyo University
orbit inclination	65 (xsd:integer)
orbit period	5539.2 (second)
orbit reference	Geocentric orbit
orbit regime	Low Earth orbit
SATCAT	39576 (xsd:integer)
website	http://www.teikyo-u.ac.jp/affiliate/teikyosat/summary.html
has abstract	TeikyoSat-3 adalah demonstrator teknologi dan mikrobiologi marbology dimaksudkan untuk penelitian siklus hidup jamur lendir pada spesies sacromontarism. TeikyoSat-3 juga mengirimkan telemetri yang uncoded di 473,45 MHz, dan setiap operator radio amatir dipersilahkan untuk berbagi data downlink. (in) TeikyoSat-3 was a technology demonstrator and microbiology microsatellite intended to research the slime mold life cycle in space. Specifically, the effects of ionizing radiation (20-30 Gy/year) are or special concern. The primary mission is expected to be finished in 10–20 days with completion of first life cycle of slime mold in space, but mission can be extended to study evolutionary adaptations for a maximum of 1 year. Also, a novel thermal control system capable of keeping a stable (10 °C to 28 °C) temperature in small (20 kg) microsatellite bus is being tested. The satellite is made in Teikyo University (Japan) and has a size of 320x320x370mm. The microsatellite microbiology experimental platform is intended to address issues with cost and uncertain future of experiments based on International Space Station.TeikyoSat-3 also transmit its telemetry uncoded at 473.45 MHz, and any amateur radio operator is welcome to share downlink data. (en)
orbit epoch	2014-02-28 (xsd:date)
gold:hypernym	Demonstrator
prov:wasDerivedFrom	wikipedia-en:TeikyoSat-3?oldid=1053178899&ns=0
page length (characters) of wiki page	3263 (xsd:nonNegativeInteger)
COSPAR id	2014-009E
landing date	2014-10-25 (xsd:date)
launch date	2014-02-27 (xsd:date)
SATCAT	39576
launch vehicle	H-IIA
manufacturer	Teikyo University
operator	Teikyo University
foaf:isPrimaryTopicOf	wikipedia-en:TeikyoSat-3
is Link from a Wikipage to another Wikipage of	2014 in spaceflight List of H-II series and H3 launches List of JAXA launches

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