About: FG-36

An Entity of Type: television show, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

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.

Property	Value
dbo: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)
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dbo:wikiPageRevisionID	1000742314 (xsd:integer)
dbo:wikiPageWikiLink	dbr:Apogee_kick_motor dbr:Geostationary_orbit dbr:Government_of_China dbr:Long_March_1D dbr:CTS_(rocket_stage) dbr:FG-15 dbr:FG-46 dbr:Fengyun dbr:Reaction_control_system dbr:Hydroxyl-terminated_polybutadiene dbc:Solid-fuel_rockets dbr:China dbr:China_Aerospace_Science_and_Industry_Corporation dbc:Rocket_engines_of_China dbr:Specific_impulse dbr:Spin-stabilisation dbr:China_Hexi_Chemical_and_Machinery_Corporation
dbp:associated	0001-03-01 (xsd:gMonthDay)
dbp:burnTime	43.0 (dbd:second)
dbp:combustionChamber	1 (xsd:integer)
dbp:countryOfOrigin	dbr:China
dbp:designer	dbr:China_Hexi_Chemical_and_Machinery_Corporation
dbp:firstDate	1986-02-02 (xsd:date)
dbp:fuel	dbr:Hydroxyl-terminated_polybutadiene
dbp:name	FG-15B (en)
dbp:predecessor	dbr:FG-15
dbp:purpose	dbr:Apogee_kick_motor
dbp:status	Out of Production (en)
dbp:successor	dbr:FG-46
dbp:type	solid (en)
dbp:usedIn	0001-03-01 (xsd:gMonthDay)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_rocket_engine dbt:Orbital_spacecraft_rocket_engines dbt:Reflist dbt:Rocket-stub dbt:Rocket_engines
dct:subject	dbc:Solid-fuel_rockets dbc:Rocket_engines_of_China
gold:hypernym	dbr:Spin
rdf:type	dbo:TelevisionShow
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)
rdfs:label	FG-36 (en)
owl:sameAs	yago-res:FG-36 wikidata:FG-36 https://global.dbpedia.org/id/2EtJG
prov:wasDerivedFrom	wikipedia-en:FG-36?oldid=1000742314&ns=0
foaf:isPrimaryTopicOf	wikipedia-en:FG-36
is dbo:wikiPageWikiLink of	dbr:Long_March_1D dbr:FG-15 dbr:Fengyun_2-05 dbr:Fengyun_2-07
is dbp:successor of	dbr:FG-15
is foaf:primaryTopic of	wikipedia-en:FG-36

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