dbo:abstract |
The HAL HTFE-25 ("Hindustan Turbo Fan Engine") is a 25 kn turbofan engine under development by Hindustan Aeronautics Limited (HAL). The engine can be used in single engine trainer jets, business jets and UAVs weighing up to 5 tonnes and in twin engine configuration for same weighing up to 9 tonnes. Based on the technical feasibility, the market potential for engine is of 200-250 units. Two engines have been produced and completed 339 runs as of 2019 out of which 96 runs were conducted in 2018-19. Engine has successfully completed cold starting test at 14 °C with spark igniters and has also achieved 100 per cent max speed with and without IGV modulation. The company has also initiated the development for integrating afterburner technology on engine. In March 2019, first test with "basic afterburner" configuration was conducted on the engine. (en) |
dbo:thumbnail |
wiki-commons:Special:FilePath/HTFE-25_turbofan_engine_from_HAL.png?width=300 |
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dbo:wikiPageWikiLink |
dbr:Rolls-Royce_Turbomeca_Adour dbr:List_of_aircraft_engines dbr:Overall_pressure_ratio dbr:NPO_Saturn_AL-55 dbr:Turbofan dbr:HAL_HTSE-1200 dbr:Hindustan_Aeronautics_Limited dbr:Afterburner dbc:Gas_turbines dbr:India dbr:Afterburning |
dbp:currentStatus |
Under development (en) |
dbp:firstRun |
2015-12-14 (xsd:date) |
dbp:lists |
* List of aircraft engines (en) |
dbp:manufacturer |
dbr:Hindustan_Aeronautics_Limited |
dbp:nationalOrigin |
dbr:India |
dbp:numberBuilt |
2 (xsd:integer) |
dbp:related |
* HAL HTSE-1200 (en) |
dbp:similarEngines |
* NPO Saturn AL-55 * Rolls-Royce Turbomeca Adour (en) |
dbp:type |
dbr:Turbofan dbr:Afterburning |
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dbt:Convert dbt:INRConvert dbt:Reflist dbt:Short_description dbt:Hindustan_Aeronautics_Limited dbt:Aircontent dbt:Infobox_aircraft_engine |
dcterms:subject |
dbc:Gas_turbines |
rdfs:comment |
The HAL HTFE-25 ("Hindustan Turbo Fan Engine") is a 25 kn turbofan engine under development by Hindustan Aeronautics Limited (HAL). The engine can be used in single engine trainer jets, business jets and UAVs weighing up to 5 tonnes and in twin engine configuration for same weighing up to 9 tonnes. Based on the technical feasibility, the market potential for engine is of 200-250 units. (en) |
rdfs:label |
HAL HTFE-25 (en) |
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yago-res:HAL HTFE-25 wikidata:HAL HTFE-25 dbpedia-tr:HAL HTFE-25 https://global.dbpedia.org/id/2LeL9 |
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wikipedia-en:HAL_HTFE-25?oldid=1123831861&ns=0 |
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wiki-commons:Special:FilePath/HTFE-25_turbofan_engine_from_HAL.png |
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wikipedia-en:HAL_HTFE-25 |
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dbr:HTFE-25 |
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dbr:List_of_aircraft_engines dbr:HTFE-25 dbr:HAL_CATS_Warrior dbr:HAL_HTSE-1200 dbr:Hindustan_Aeronautics_Limited dbr:Ivchenko-Progress_AI-222 dbr:Ivchenko-Progress_AI-322 |
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dbr:HAL_CATS_Warrior |
is foaf:primaryTopic of |
wikipedia-en:HAL_HTFE-25 |