Properties (109)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:aircraft |
gptkb:Dassault_Mirage_2000-5
gptkb:Mirage_2000 gptkb:Dassault_Mirage_2000D HAL Tejas Dassault Mirage 2000-10 Mirage_family Dassault_Mirage_2000-1 Dassault_Mirage_2000-11 Dassault_Mirage_2000-12 Dassault_Mirage_2000-13 Dassault_Mirage_2000-14 Dassault_Mirage_2000-15 Dassault_Mirage_2000-16 Dassault_Mirage_2000-17 Dassault_Mirage_2000-18 Dassault_Mirage_2000-19 Dassault_Mirage_2000-2 Dassault_Mirage_2000-20 Dassault_Mirage_2000-21 Dassault_Mirage_2000-22 Dassault_Mirage_2000-23 Dassault_Mirage_2000-24 Dassault_Mirage_2000-25 Dassault_Mirage_2000-26 Dassault_Mirage_2000-27 Dassault_Mirage_2000-28 Dassault_Mirage_2000-29 Dassault_Mirage_2000-3 Dassault_Mirage_2000-30 Dassault_Mirage_2000-31 Dassault_Mirage_2000-32 Dassault_Mirage_2000-33 Dassault_Mirage_2000-34 Dassault_Mirage_2000-35 Dassault_Mirage_2000-36 Dassault_Mirage_2000-37 Dassault_Mirage_2000-38 Dassault_Mirage_2000-39 Dassault_Mirage_2000-4 Dassault_Mirage_2000-40 Dassault_Mirage_2000-41 Dassault_Mirage_2000-42 Dassault_Mirage_2000-43 Dassault_Mirage_2000-44 Dassault_Mirage_2000-45 Dassault_Mirage_2000-46 Dassault_Mirage_2000-47 Dassault_Mirage_2000-48 Dassault_Mirage_2000-49 Dassault_Mirage_2000-50 Dassault_Mirage_2000-7 Dassault_Mirage_2000-8 Dassault_Mirage_2000-9 Dassault_Mirage_2000C Dassault_Mirage_2000N SEPECAT_Jaguar |
| gptkbp:application |
military aircraft
|
| gptkbp:controls |
FADEC
|
| gptkbp:developer |
Snecma_M53-P2
|
| gptkbp:diameter |
0.9 m
about 0.9 m |
| gptkbp:emissionsStandard |
compliant_with_ICAO_standards
|
| gptkbp:engine |
0.9 m
4.2 m state-of-the-art technology 1,200 lb various military applications Snecma_design_team |
| gptkbp:engineConfiguration |
ongoing
twin-spool military jet engine market |
| gptkbp:engineType |
gptkb:M53-P2
advanced aerodynamics turbofan axial air start single-stage high-pressure turbine |
| gptkbp:firstFlight |
1978
|
| gptkbp:fuel_capacity |
0.8 kg/kN·h
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular |
| gptkbp:hasArea |
extensive testing conducted
certified_by_French_authorities |
| https://www.w3.org/2000/01/rdf-schema#label |
Snecma M53
|
| gptkbp:is_used_in |
gptkb:Dassault_Mirage_2000
|
| gptkbp:length |
3.8 m
about 4.2 m |
| gptkbp:maintenance |
1,000 hours
|
| gptkbp:manufacturer |
gptkb:Snecma
|
| gptkbp:maximum_speed |
gptkb:Mach_2.2
|
| gptkbp:noise_level |
low noise
|
| gptkbp:notable_feature |
high thrust-to-weight ratio
|
| gptkbp:operational_status |
gptkb:French_Air_Force
|
| gptkbp:origin |
gptkb:France
|
| gptkbp:performances |
high performance
high reliability |
| gptkbp:productionYears |
1970s
|
| gptkbp:propulsion |
no
around 9,000 lbf |
| gptkbp:related_engine |
Brayton_cycle
Snecma_M53-P2 |
| gptkbp:reviews |
9,000 lbf
|
| gptkbp:service_ceiling |
60,000 ft
|
| gptkbp:successor |
gptkb:Snecma_M88
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:updates |
upgraded versions available
|
| gptkbp:weight |
about 1,200 kg
about 1,200 lb |