About: FG-36

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An Entity of Type : dbo:TelevisionShow, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
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The FG-36 (AKA Fengyun 2 AKM) was a Chinese spin stabilized apogee kick motor burning HTPB. It was developed by (also known as the 6th Academy of CASIC) for use in the Fengyun 2 satellite bus for insertion into GSO orbit.

Attributes	Values
rdf:type	television show
rdfs:label	FG-36 (en)
rdfs:comment	The FG-36 (AKA Fengyun 2 AKM) was a Chinese spin stabilized apogee kick motor burning HTPB. It was developed by (also known as the 6th Academy of CASIC) for use in the Fengyun 2 satellite bus for insertion into GSO orbit. (en)
name	FG-15B (en)
dcterms:subject	Solid-fuel rockets Rocket engines of China
Wikipage page ID	47365654 (xsd:integer)
Wikipage revision ID	1000742314 (xsd:integer)
Link from a Wikipage to another Wikipage	Apogee kick motor Geostationary orbit Government of China Long March 1D CTS (rocket stage) FG-15 FG-46 Fengyun Reaction control system Hydroxyl-terminated polybutadiene Solid-fuel rockets China China Aerospace Science and Industry Corporation Rocket engines of China Specific impulse Spin-stabilisation dbr:China_Hexi_Chemical_and_Machinery_Corporation
sameAs	FG-36 FG-36 FG-36
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_rocket_engine dbt:Orbital_spacecraft_rocket_engines dbt:Reflist dbt:Rocket-stub dbt:Rocket_engines
combustion chamber	1 (xsd:integer)
country of origin	China
designer	dbr:China_Hexi_Chemical_and_Machinery_Corporation
first date	1986-02-02 (xsd:date)
fuel	Hydroxyl-terminated polybutadiene
predecessor	FG-15
purpose	Apogee kick motor
status	Out of Production (en)
successor	FG-46
type	solid (en)
used in	0001-03-01 (xsd:gMonthDay)
has abstract	The FG-36 (AKA Fengyun 2 AKM) was a Chinese spin stabilized apogee kick motor burning HTPB. It was developed by (also known as the 6th Academy of CASIC) for use in the Fengyun 2 satellite bus for insertion into GSO orbit. It has a total nominal mass of 729 kg (1,607 lb), of which 650 kg (1,430 lb) is propellant load and its burn out mass is 79 kg (174 lb). It has an average thrust of 44 kN (9,900 lbf) with a specific impulse of 289 seconds burning for 43 seconds, with a total impulse of 1.842 MN (414,000 lbf). While it was designed as an apogee kick motor and as such it flew in spin stabilized mode, it was also adapted to the Long March 1D third stage. It was paired with a RCS in a similar solution to the CTS. (en)
associated	0001-03-01 (xsd:gMonthDay)
burn time	43.0 (second)
gold:hypernym	Spin
prov:wasDerivedFrom	wikipedia-en:FG-36?oldid=1000742314&ns=0
page length (characters) of wiki page	4537 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:FG-36
is Link from a Wikipage to another Wikipage of	Long March 1D FG-15 Fengyun 2-05 Fengyun 2-07
is successor of	FG-15
is foaf:primaryTopic of	wikipedia-en:FG-36

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