Honeywell AGT1500 gas turbine engine
GPTKB entity
Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gas turbine engine
|
| gptkbp:application |
military vehicle
|
| gptkbp:controls |
digital control system
|
| gptkbp:coolingSystem |
air-cooled
water-based coolant |
| gptkbp:design |
military applications
|
| gptkbp:diameter |
22 inches
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissionsStandard |
EPA_Tier_2
|
| gptkbp:energyEfficiency |
0.5 miles per gallon
|
| gptkbp:engine |
advanced technology
30 seconds liquid cooling innovative design low noise 15 seconds low vibration flexible mount 3,000 ft-lb adaptable to various applications |
| gptkbp:engineConfiguration |
gptkb:full_authority_digital_engine_control_(FADEC)
modular design inline engine |
| gptkbp:engineType |
high availability
high durability high performance high reliability low maintenance axial compressor single-stage turbine |
| gptkbp:firstFlight |
1980
|
| gptkbp:fuelCapacity |
300 gallons
0.5 gallons per hour |
| gptkbp:fuelType |
spark ignition
JP-8 annular combustion chamber multi-fuel system |
| gptkbp:generator |
1,200 °F
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell AGT1500 gas turbine engine
|
| gptkbp:launchSite |
starter motor
|
| gptkbp:length |
60 inches
|
| gptkbp:maintenance |
1,000 hours
|
| gptkbp:manufacturer |
gptkb:Honeywell
|
| gptkbp:noise_level |
85 dB
|
| gptkbp:operationalStatus |
1,500 °F
30 psi |
| gptkbp:performances |
5,000 hours
|
| gptkbp:powerOutput |
1500 horsepower
|
| gptkbp:propulsion |
3,000 pounds
1 hp/lb turbo-propulsion |
| gptkbp:services |
15,000 feet
|
| gptkbp:type |
turbojet engine
|
| gptkbp:usedIn |
gptkb:M1_Abrams_tank
|
| gptkbp:weight |
1,500 pounds
|