| dbo:abstract |
The SCE-200 is a liquid-fuel rocket engine being developed by Liquid Propulsion Systems Centre of Indian Space Research Organisation. Burning liquid oxygen (LOX) and RP-1 kerosene in an oxidizer-rich staged combustion cycle, the engine will boost payload capacity of India's existing LVM3 replacing current L110 stage powered by 2 Vikas engines. It is also expected to power ISRO's upcoming NGLV rockets (previously planned as ULV) as well as ISRO's future reusable rockets based on RLV technology demonstrations. The engine in September 2019 reportedly had become ready to begin testing in Ukraine and enter service no earlier than 2022. The use of engine of India's first human spaceflight, hence was ruled out by ISRO. By November 2022, SCE-200 had neared completion of its qualification tests. Stage and development had been complete and a facility to test it at ISRO Propulsion Complex Mahendergiri was getting ready for ground tests. (en) SCE-200은 인도 ISRO가 개발중인 추력 200톤급 등유/액체산소 로켓 엔진이다. (ko) SCE-200はISRO傘下の液体推進システムセンターで開発中の液体燃料 ロケットエンジンである。ISROによって予定される将来の重量物打ち上げ用のUnified Launch Vehicle (ULV)と (RLV)の動力のために開発中であるが 、その前にGSLV Mk IIIの(古いヴィカースエンジンを動力とする)L110 ステージを SC160に置き換えて試験する予定である。 第一のISROの目標はULV (Unified Launch Vehicle)と呼ばれる新しいSLVシリーズで現行のPSLV、GSLVとGSLV Mk IIIを置き換える事である。ULV (Unified Launch Vehicle)は人工衛星打ち上げ機の推進剤としてN2O4/UDMHを放棄した。 (ja) O SCE-200 é um motor de foguete de combustível líquido indiano em desenvolvimento, queimando LOX e RP-1 num ciclo de combustão em estágios rico em oxidante. Esse motor deve equipar os futuros Unified Launch Vehicle (ULV) e da Organização Indiana de Pesquisa Espacial. Ele vai ser testado primeiramente num GSLV Mk III substituindo o estágio L110 com o motor Vikas por um estágio SC-200 com um motor SCE-200 e 200 toneladas de propelentes. (pt) |
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dbr:Ukraine dbr:Unified_Launch_Vehicle dbr:Vikas_(rocket_engine) dbr:Memorandum_of_Understanding dbr:Russian_Federal_Space_Agency dbr:Gaganyaan dbr:Geostationary_transfer_orbit dbr:Godrej_&_Boyce dbr:Liquid_Propulsion_Systems_Centre dbr:Yuzhmash dbr:Yuzhnoye_Design_Office dbr:WikiLeaks dbr:Liquid_oxygen dbr:Geosynchronous_Satellite_Launch_Vehicle_Mk_III dbr:A._S._Kiran_Kumar dbc:Rocket_engines_using_kerosene_propellant dbc:Rocket_engines_using_the_staged_combustion_cycle dbr:Staged_combustion_cycle_(rocket) dbc:Rocket_engines_of_India dbr:ISRO_Propulsion_Complex dbr:India dbr:Indian_Space_Research_Organisation dbr:RD-120 dbr:RD-170 dbr:RD-810 dbr:RLV-TD dbr:RP-1 dbr:RLV_Technology_Demonstration_Programme dbr:LOX dbr:Staged_combustion_cycle dbr:Rocket_engine dbr:LVM3 dbr:Liquid-fuel_rocket |
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1 (xsd:integer) |
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dbr:India |
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dbr:Staged_combustion_cycle_(rocket) |
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dbr:Liquid_Propulsion_Systems_Centre dbr:Indian_Space_Research_Organisation |
| dbp:dryWeight |
~2700 kg (en) |
| dbp:fuel |
dbr:RP-1 |
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dbr:Godrej_&_Boyce |
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2.650000 (xsd:double) |
| dbp:name |
SCE-200 (en) |
| dbp:oxidiser |
dbr:LOX |
| dbp:purpose |
Main engine (en) |
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Under Development (en) |
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60 (xsd:integer) |
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liquid (en) |
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dbr:Engine |
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dbo:Software |
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SCE-200은 인도 ISRO가 개발중인 추력 200톤급 등유/액체산소 로켓 엔진이다. (ko) SCE-200はISRO傘下の液体推進システムセンターで開発中の液体燃料 ロケットエンジンである。ISROによって予定される将来の重量物打ち上げ用のUnified Launch Vehicle (ULV)と (RLV)の動力のために開発中であるが 、その前にGSLV Mk IIIの(古いヴィカースエンジンを動力とする)L110 ステージを SC160に置き換えて試験する予定である。 第一のISROの目標はULV (Unified Launch Vehicle)と呼ばれる新しいSLVシリーズで現行のPSLV、GSLVとGSLV Mk IIIを置き換える事である。ULV (Unified Launch Vehicle)は人工衛星打ち上げ機の推進剤としてN2O4/UDMHを放棄した。 (ja) O SCE-200 é um motor de foguete de combustível líquido indiano em desenvolvimento, queimando LOX e RP-1 num ciclo de combustão em estágios rico em oxidante. Esse motor deve equipar os futuros Unified Launch Vehicle (ULV) e da Organização Indiana de Pesquisa Espacial. Ele vai ser testado primeiramente num GSLV Mk III substituindo o estágio L110 com o motor Vikas por um estágio SC-200 com um motor SCE-200 e 200 toneladas de propelentes. (pt) The SCE-200 is a liquid-fuel rocket engine being developed by Liquid Propulsion Systems Centre of Indian Space Research Organisation. Burning liquid oxygen (LOX) and RP-1 kerosene in an oxidizer-rich staged combustion cycle, the engine will boost payload capacity of India's existing LVM3 replacing current L110 stage powered by 2 Vikas engines. It is also expected to power ISRO's upcoming NGLV rockets (previously planned as ULV) as well as ISRO's future reusable rockets based on RLV technology demonstrations. (en) |
| rdfs:label |
SCE-200 (ko) SCE-200 (ja) SCE-200 (en) SCE-200 (pt) |
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freebase:SCE-200 yago-res:SCE-200 wikidata:SCE-200 http://hi.dbpedia.org/resource/सेमी_क्रायोजेनिक_इंजन-200 dbpedia-ja:SCE-200 dbpedia-ko:SCE-200 dbpedia-pt:SCE-200 https://global.dbpedia.org/id/s66j |
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wikipedia-en:SCE-200?oldid=1123070812&ns=0 |
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wikipedia-en:SCE-200 |
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wikipedia-en:SCE-200 |