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- FG-36 abstract "The FG-36 (AKA Fengyun 2 AKM) was a Chinese spin stabilized apogee kick motor burning HTPB. It was developed by China Hexi Chemical and Machinery Corporation (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.".
- FG-36 wikiPageID "47365654".
- FG-36 wikiPageLength "4303".
- FG-36 wikiPageOutDegree "28".
- FG-36 wikiPageRevisionID "675949102".
- FG-36 wikiPageWikiLink Apogee_kick_motor.
- FG-36 wikiPageWikiLink CTS_(rocket_stage).
- FG-36 wikiPageWikiLink Category:Rocket_engines.
- FG-36 wikiPageWikiLink Category:Rocket_engines_of_China.
- FG-36 wikiPageWikiLink Category:Solid-fuel_rockets.
- FG-36 wikiPageWikiLink China.
- FG-36 wikiPageWikiLink China_Aerospace_Science_and_Industry_Corporation.
- FG-36 wikiPageWikiLink China_Hexi_Chemical_and_Machinery_Corporation.
- FG-36 wikiPageWikiLink FG-15.
- FG-36 wikiPageWikiLink FG-46.
- FG-36 wikiPageWikiLink Fengyun.
- FG-36 wikiPageWikiLink Geostationary_orbit.
- FG-36 wikiPageWikiLink Government_of_China.
- FG-36 wikiPageWikiLink Hydroxyl-terminated_polybutadiene.
- FG-36 wikiPageWikiLink Long_March_1D.
- FG-36 wikiPageWikiLink Reaction_control_system.
- FG-36 wikiPageWikiLink Specific_impulse.
- FG-36 wikiPageWikiLink Spin-stabilisation.
- FG-36 wikiPageWikiLinkText "FG-36".
- FG-36 associated "--03-01".
- FG-36 burnTime "43.0".
- FG-36 combustionChamber "1".
- FG-36 countryOfOrigin China.
- FG-36 designer China_Hexi_Chemical_and_Machinery_Corporation.
- FG-36 firstDate "1986-02-02".
- FG-36 fuel Hydroxyl-terminated_polybutadiene.
- FG-36 name "FG-15B".
- FG-36 predecessor FG-15.
- FG-36 purpose Apogee_kick_motor.
- FG-36 status "Out of Production".
- FG-36 successor FG-46.
- FG-36 type "solid".
- FG-36 usedIn "--03-01".
- FG-36 wikiPageUsesTemplate Template:Convert.
- FG-36 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- FG-36 wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- FG-36 wikiPageUsesTemplate Template:Reflist.
- FG-36 wikiPageUsesTemplate Template:Rocket-stub.
- FG-36 wikiPageUsesTemplate Template:Rocket_Engines.
- FG-36 subject Category:Rocket_engines.
- FG-36 subject Category:Rocket_engines_of_China.
- FG-36 subject Category:Solid-fuel_rockets.
- FG-36 hypernym Spin.
- FG-36 type TelevisionShow.
- FG-36 comment "The FG-36 (AKA Fengyun 2 AKM) was a Chinese spin stabilized apogee kick motor burning HTPB. It was developed by China Hexi Chemical and Machinery Corporation (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).".
- FG-36 label "FG-36".
- FG-36 wasDerivedFrom FG-36?oldid=675949102.
- FG-36 isPrimaryTopicOf FG-36.