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- FG-47 abstract "The FG-47 (AKA SpaB-54) is a Chinese solid rocket 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 Long March 2C SD/CTS/SMA third stage. It had its inaugural flight on the Iridium-MFS demonstration mission on September 1, 1997.It has a total nominal mass of 160 kg (350 lb), of which 125 kg (276 lb) is propellant load. It has an average thrust of 9.8 kN (2,200 lbf) with a specific impulse of 288 seconds burning for 35 seconds, with a total impulse of 353 kN (79,000 lbf).".
- FG-47 wikiPageID "47339067".
- FG-47 wikiPageLength "4072".
- FG-47 wikiPageOutDegree "22".
- FG-47 wikiPageRevisionID "692787734".
- FG-47 wikiPageWikiLink CTS_(rocket_stage).
- FG-47 wikiPageWikiLink Category:Rocket_engines.
- FG-47 wikiPageWikiLink Category:Rocket_engines_of_China.
- FG-47 wikiPageWikiLink Category:Solid-fuel_rockets.
- FG-47 wikiPageWikiLink China.
- FG-47 wikiPageWikiLink China_Aerospace_Science_and_Industry_Corporation.
- FG-47 wikiPageWikiLink China_Hexi_Chemical_and_Machinery_Corporation.
- FG-47 wikiPageWikiLink Government_of_China.
- FG-47 wikiPageWikiLink Hydroxyl-terminated_polybutadiene.
- FG-47 wikiPageWikiLink Iridium_satellite_constellation.
- FG-47 wikiPageWikiLink Long_March_2C.
- FG-47 wikiPageWikiLink Rocket_engine.
- FG-47 wikiPageWikiLink Solid-fuel_rocket.
- FG-47 wikiPageWikiLink Specific_impulse.
- FG-47 wikiPageWikiLinkText "FG-47".
- FG-47 associated "--03-02".
- FG-47 burnTime "36.0".
- FG-47 countryOfOrigin China.
- FG-47 designer China_Hexi_Chemical_and_Machinery_Corporation.
- FG-47 firstDate "1997-09-01".
- FG-47 fuel Hydroxyl-terminated_polybutadiene.
- FG-47 name "FG-47".
- FG-47 purpose "Kick engine".
- FG-47 status "In Production".
- FG-47 type "solid".
- FG-47 usedIn CTS_(rocket_stage).
- FG-47 wikiPageUsesTemplate Template:Convert.
- FG-47 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- FG-47 wikiPageUsesTemplate Template:Reflist.
- FG-47 wikiPageUsesTemplate Template:Rocket-stub.
- FG-47 wikiPageUsesTemplate Template:Rocket_Engines.
- FG-47 subject Category:Rocket_engines.
- FG-47 subject Category:Rocket_engines_of_China.
- FG-47 subject Category:Solid-fuel_rockets.
- FG-47 hypernym HTPB.
- FG-47 comment "The FG-47 (AKA SpaB-54) is a Chinese solid rocket 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 Long March 2C SD/CTS/SMA third stage. It had its inaugural flight on the Iridium-MFS demonstration mission on September 1, 1997.It has a total nominal mass of 160 kg (350 lb), of which 125 kg (276 lb) is propellant load.".
- FG-47 label "FG-47".
- FG-47 wasDerivedFrom FG-47?oldid=692787734.
- FG-47 isPrimaryTopicOf FG-47.