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Statements

Subject Item
dbr:FG-36
rdf:type
dbo:TelevisionShow
rdfs:label
FG-36
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.
dbp:name
FG-15B
dct:subject
dbc:Rocket_engines_of_China dbc:Solid-fuel_rockets
dbo:wikiPageID
47365654
dbo:wikiPageRevisionID
1000742314
dbo:wikiPageWikiLink
dbr:China_Hexi_Chemical_and_Machinery_Corporation dbr:Apogee_kick_motor dbr:Fengyun dbr:Reaction_control_system dbr:Government_of_China dbr:Hydroxyl-terminated_polybutadiene dbr:CTS_(rocket_stage) dbr:Specific_impulse dbr:FG-15 dbr:Geostationary_orbit dbc:Rocket_engines_of_China dbr:FG-46 dbr:China dbr:Spin-stabilisation dbr:China_Aerospace_Science_and_Industry_Corporation dbr:Long_March_1D dbc:Solid-fuel_rockets
owl:sameAs
n4:2EtJG yago-res:FG-36 wikidata:Q23777534
dbp:wikiPageUsesTemplate
dbt:Convert dbt:Orbital_spacecraft_rocket_engines dbt:Infobox_rocket_engine dbt:Rocket-stub dbt:Rocket_engines dbt:Reflist
dbp:combustionChamber
1
dbp:countryOfOrigin
dbr:China
dbp:designer
dbr:China_Hexi_Chemical_and_Machinery_Corporation
dbp:firstDate
1986-02-02
dbp:fuel
dbr:Hydroxyl-terminated_polybutadiene
dbp:predecessor
dbr:FG-15
dbp:purpose
dbr:Apogee_kick_motor
dbp:status
Out of Production
dbp:successor
dbr:FG-46
dbp:type
solid
dbp:usedIn
0001-03-01
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.
dbp:associated
0001-03-01
dbp:burnTime
43.0
gold:hypernym
dbr:Spin
prov:wasDerivedFrom
wikipedia-en:FG-36?oldid=1000742314&ns=0
dbo:wikiPageLength
4537
foaf:isPrimaryTopicOf
wikipedia-en:FG-36