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- FG-02 abstract "The FG-02 was a Chinese solid rocket motor burning Polysulfide. It was developed by China Hexi Chemical and Machinery Corporation (also known as the 6th Academy of CASIC) for use in the Long March 1 third stage. It has a total nominal mass of 2,052 kg (4,524 lb), of which 1,806 kg (3,982 lb) is propellant load. It has an average thrust of 181 kN (41,000 lbf) with a specific impulse of 254 seconds burning for 38 seconds, with a total impulse of 4,500 kN (1,000,000 lbf). It used spin stabilization and a timing device to ignite in flight.The Long March 1 is basically a DF-4 with a solid third stage and a fairing. So the FG-02 was developed as the third stage to add to the stack. It was initially tested on two launches aboard T-7A sounding rockets to validate high altitude ignitions. Both successful flights were performed on August 1968. Before going into the launch vehicle, the propellant load was increased from 900 kg (2,000 lb) to 1,806 kg (3,982 lb). It performed just two orbital flights, both from Jiuquan and both successful. The first was on April 14, 1970, to orbit the indigenous satellite, the Dong Fang Hong I. And the second was on March 3, 1971, on the Shijian 1 mission.".
- FG-02 wikiPageID "47360936".
- FG-02 wikiPageLength "4141".
- FG-02 wikiPageOutDegree "25".
- FG-02 wikiPageRevisionID "694367222".
- FG-02 wikiPageWikiLink Category:Rocket_engines.
- FG-02 wikiPageWikiLink Category:Rocket_engines_of_China.
- FG-02 wikiPageWikiLink Category:Rocket_stages.
- FG-02 wikiPageWikiLink Category:Solid-fuel_rockets.
- FG-02 wikiPageWikiLink China.
- FG-02 wikiPageWikiLink China_Aerospace_Science_and_Industry_Corporation.
- FG-02 wikiPageWikiLink China_Hexi_Chemical_and_Machinery_Corporation.
- FG-02 wikiPageWikiLink DF-4.
- FG-02 wikiPageWikiLink Dong_Fang_Hong_I.
- FG-02 wikiPageWikiLink Government_of_China.
- FG-02 wikiPageWikiLink Jiuquan_Satellite_Launch_Center.
- FG-02 wikiPageWikiLink Long_March_1.
- FG-02 wikiPageWikiLink Polysulfide.
- FG-02 wikiPageWikiLink Rocket_engine.
- FG-02 wikiPageWikiLink Shijian_1.
- FG-02 wikiPageWikiLink Solid-fuel_rocket.
- FG-02 wikiPageWikiLink Specific_impulse.
- FG-02 wikiPageWikiLink Spin-stabilisation.
- FG-02 wikiPageWikiLinkText "FG-02".
- FG-02 associated "--03-01".
- FG-02 burnTime "38.0".
- FG-02 combustionChamber "1".
- FG-02 countryOfOrigin China.
- FG-02 date "1966".
- FG-02 designer China_Hexi_Chemical_and_Machinery_Corporation.
- FG-02 firstDate "1970-04-24".
- FG-02 fuel Polysulfide.
- FG-02 lastDate "1971-03-03".
- FG-02 name "FG-02".
- FG-02 purpose "Upper stage".
- FG-02 status "Retired".
- FG-02 type "solid".
- FG-02 usedIn "--03-01".
- FG-02 wikiPageUsesTemplate Template:Convert.
- FG-02 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- FG-02 wikiPageUsesTemplate Template:Reflist.
- FG-02 wikiPageUsesTemplate Template:Rocket-stub.
- FG-02 wikiPageUsesTemplate Template:Rocket_Engines.
- FG-02 wikiPageUsesTemplate Template:Upper_stages.
- FG-02 subject Category:Rocket_engines.
- FG-02 subject Category:Rocket_engines_of_China.
- FG-02 subject Category:Rocket_stages.
- FG-02 subject Category:Solid-fuel_rockets.
- FG-02 hypernym Polysulfide.
- FG-02 comment "The FG-02 was a Chinese solid rocket motor burning Polysulfide. It was developed by China Hexi Chemical and Machinery Corporation (also known as the 6th Academy of CASIC) for use in the Long March 1 third stage. It has a total nominal mass of 2,052 kg (4,524 lb), of which 1,806 kg (3,982 lb) is propellant load. It has an average thrust of 181 kN (41,000 lbf) with a specific impulse of 254 seconds burning for 38 seconds, with a total impulse of 4,500 kN (1,000,000 lbf).".
- FG-02 label "FG-02".
- FG-02 sameAs Q21714922.
- FG-02 sameAs FG-02.
- FG-02 sameAs Q21714922.
- FG-02 wasDerivedFrom FG-02?oldid=694367222.
- FG-02 isPrimaryTopicOf FG-02.