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- FG-46 abstract "The FG-46 (AKA EPKM and SpaB-170) is a Chinese spin stabilized 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 2E on GTO missions. It first flew as a prototype PKM on July 16, 1990 on the Badr A mission. It had its first commercial mission orbiting the AsiaSat 2 on November 28, 1995 and exactly one month later, on December 28 its second and last mission for EchoStar 1.It has a total nominal mass of 6,001 kg (13,230 lb), of which 5,444 kg (12,002 lb) is propellant load and its burn out mass is 529 kg (1,166 lb). It has an average thrust of 190 kN (43,000 lbf) with a specific impulse of 292 seconds burning for 87 seconds, with a total impulse of 1.589 MN (357,000 lbf). It is spin stabilized at 40 rpm and the propellant mass can be reduced by up to 350 kg (770 lb) eight months before launch or up to 15 kg (33 lb) on the launch site.".
- FG-46 wikiPageID "47336979".
- FG-46 wikiPageLength "4262".
- FG-46 wikiPageOutDegree "23".
- FG-46 wikiPageRevisionID "692787715".
- FG-46 wikiPageWikiLink AsiaSat_2.
- FG-46 wikiPageWikiLink Badr_A.
- FG-46 wikiPageWikiLink Category:Rocket_engines.
- FG-46 wikiPageWikiLink Category:Rocket_engines_of_China.
- FG-46 wikiPageWikiLink Category:Solid-fuel_rockets.
- FG-46 wikiPageWikiLink China.
- FG-46 wikiPageWikiLink China_Aerospace_Science_and_Industry_Corporation.
- FG-46 wikiPageWikiLink China_Hexi_Chemical_and_Machinery_Corporation.
- FG-46 wikiPageWikiLink EchoStar_1.
- FG-46 wikiPageWikiLink Fiberglass.
- FG-46 wikiPageWikiLink Geostationary_transfer_orbit.
- FG-46 wikiPageWikiLink Government_of_China.
- FG-46 wikiPageWikiLink Hydroxyl-terminated_polybutadiene.
- FG-46 wikiPageWikiLink Long_March_2E.
- FG-46 wikiPageWikiLink Revolutions_per_minute.
- FG-46 wikiPageWikiLink Rocket_engine.
- FG-46 wikiPageWikiLink Solid-fuel_rocket.
- FG-46 wikiPageWikiLink Specific_impulse.
- FG-46 wikiPageWikiLink Spin-stabilisation.
- FG-46 wikiPageWikiLinkText "FG-46".
- FG-46 associated "--03-02".
- FG-46 burnTime "87.0".
- FG-46 casing Fiberglass.
- FG-46 countryOfOrigin China.
- FG-46 designer China_Hexi_Chemical_and_Machinery_Corporation.
- FG-46 firstDate "1995-11-28".
- FG-46 fuel Hydroxyl-terminated_polybutadiene.
- FG-46 name "FG-46".
- FG-46 purpose "Kick engine".
- FG-46 status "Out of Production".
- FG-46 type "solid".
- FG-46 usedIn "--03-02".
- FG-46 wikiPageUsesTemplate Template:Convert.
- FG-46 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- FG-46 wikiPageUsesTemplate Template:Reflist.
- FG-46 wikiPageUsesTemplate Template:Rocket-stub.
- FG-46 wikiPageUsesTemplate Template:Rocket_Engines.
- FG-46 subject Category:Rocket_engines.
- FG-46 subject Category:Rocket_engines_of_China.
- FG-46 subject Category:Solid-fuel_rockets.
- FG-46 hypernym Spin.
- FG-46 type TelevisionShow.
- FG-46 comment "The FG-46 (AKA EPKM and SpaB-170) is a Chinese spin stabilized 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 2E on GTO missions. It first flew as a prototype PKM on July 16, 1990 on the Badr A mission.".
- FG-46 label "FG-46".
- FG-46 sameAs Q21717776.
- FG-46 sameAs FG-46.
- FG-46 sameAs Q21717776.
- FG-46 wasDerivedFrom FG-46?oldid=692787715.
- FG-46 isPrimaryTopicOf FG-46.