FG-47 (original) (raw)
The FG-47 (a.k.a. SpaB-54) is a Chinese solid rocket motor burning HTPB. It was developed by (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).
| Property | Value |
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| dbo:abstract | The FG-47 (a.k.a. SpaB-54) is a Chinese solid rocket motor burning HTPB. It was developed by (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). (en) El FG-47 (también conocido como SpaB-54) es un cohete de combustible sólido chino que quema polibutadenio terminado en hidroxilo. Fue desarrollado por China Hexi Chemical and Machinery Corporation (también conocida como la sexta academia de CASIC) para usarlo en la tercera etapa del Long March 2C SD/CTS/SMA. Tuvo su vuelo inaugural en la misión de demostración del Iridium-MFS el 1 de septiembre de 1997. Tiene una masa nominal total de 160 kg, de los cuales 125 kg es carga propulsora. Tiene un empuje aproximado de 9.8 kN con un impulso específico de 288 segundos ardiendo durante 35 segundos, con un impulso total de 353 kN. (es) |
| dbo:wikiPageID | 47339067 (xsd:integer) |
| dbo:wikiPageLength | 4516 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID | 1032573607 (xsd:integer) |
| dbo:wikiPageWikiLink | dbr:Government_of_China dbr:Long_March_2C dbr:CTS_(rocket_stage) dbr:Solid-fuel_rocket dbr:Iridium_satellite_constellation dbr:Hydroxyl-terminated_polybutadiene dbc:Solid-fuel_rockets dbr:China dbr:China_Aerospace_Science_and_Industry_Corporation dbc:Rocket_engines_of_China dbr:Specific_impulse dbr:Rocket_engine dbr:China_Hexi_Chemical_and_Machinery_Corporation |
| dbp:associated | 0001-03-02 (xsd:gMonthDay) |
| dbp:burnTime | 36.0 |
| dbp:countryOfOrigin | dbr:China |
| dbp:designer | dbr:China_Hexi_Chemical_and_Machinery_Corporation |
| dbp:firstDate | 1997-09-01 (xsd:date) |
| dbp:fuel | dbr:Hydroxyl-terminated_polybutadiene |
| dbp:name | FG-47 (en) |
| dbp:purpose | Kick engine (en) |
| dbp:status | In Production (en) |
| dbp:type | solid (en) |
| dbp:usedIn | dbr:CTS_(rocket_stage) |
| dbp:wikiPageUsesTemplate | dbt:Convert dbt:Infobox_rocket_engine dbt:Reflist dbt:Rocket-stub dbt:Rocket_engines |
| dcterms:subject | dbc:Solid-fuel_rockets dbc:Rocket_engines_of_China |
| gold:hypernym | dbr:HTPB |
| rdfs:comment | The FG-47 (a.k.a. SpaB-54) is a Chinese solid rocket motor burning HTPB. It was developed by (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). (en) El FG-47 (también conocido como SpaB-54) es un cohete de combustible sólido chino que quema polibutadenio terminado en hidroxilo. Fue desarrollado por China Hexi Chemical and Machinery Corporation (también conocida como la sexta academia de CASIC) para usarlo en la tercera etapa del Long March 2C SD/CTS/SMA. Tuvo su vuelo inaugural en la misión de demostración del Iridium-MFS el 1 de septiembre de 1997. (es) |
| rdfs:label | FG-47 (en) FG-47 (es) |
| owl:sameAs | yago-res:FG-47 wikidata:FG-47 dbpedia-es:FG-47 https://global.dbpedia.org/id/2F9jM |
| prov:wasDerivedFrom | wikipedia-en:FG-47?oldid=1032573607&ns=0 |
| foaf:isPrimaryTopicOf | wikipedia-en:FG-47 |
| is dbo:wikiPageWikiLink of | dbr:CTS_(rocket_stage) |
| is foaf:primaryTopic of | wikipedia-en:FG-47 |