Honeywell AGT1500 gas turbine engine
GPTKB entity
Statements (59)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:military_vehicles
|
| gptkbp:average_temperature |
up to 1,500 degrees Fahrenheit
high turbine inlet temperature |
| gptkbp:combustor_type |
annular combustion chamber
|
| gptkbp:compression_ratio |
15:1
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control |
| gptkbp:cooling_system |
air-cooled
air as coolant |
| gptkbp:design_purpose |
military applications
|
| gptkbp:development |
1970s
|
| gptkbp:diameter |
approximately 20 inches
single-spool |
| gptkbp:elevation |
operates at high altitudes
|
| gptkbp:emissions_standard |
meets military standards
|
| gptkbp:enforces |
complies with military regulations
|
| gptkbp:engine |
high availability
active user community innovative technology comprehensive documentation ongoing research and development extensive support network |
| gptkbp:engine_configuration |
modular design
flexible mounting system compact configuration |
| gptkbp:engine_power |
high performance
high reliability up to 30,000 RPM |
| gptkbp:engine_upgrade_potential |
upgradeable design
|
| gptkbp:environmental_impact |
designed for reduced environmental impact
|
| gptkbp:first_flight |
gptkb:1980
|
| gptkbp:fuel_economy |
high efficiency
low fuel consumption |
| gptkbp:fuel_type |
gptkb:JP-8
dual fuel system |
| gptkbp:gearbox |
reduction gearbox
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell AGT1500 gas turbine engine
|
| gptkbp:ignition_system |
spark ignition
|
| gptkbp:is_tested_for |
extensively tested
state-of-the-art testing facilities |
| gptkbp:launch_window |
air start
|
| gptkbp:length |
approximately 60 inches
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
gptkb:Honeywell
|
| gptkbp:material |
advanced materials
|
| gptkbp:noise_level |
low noise emissions
|
| gptkbp:power_output |
1500 horsepower
|
| gptkbp:propulsion |
high power-to-weight ratio
3,000 pounds-force |
| gptkbp:service |
approximately 5,000 hours
|
| gptkbp:training |
training programs available
|
| gptkbp:turbine_type |
axial turbine
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:M1_Abrams_tank
|
| gptkbp:weight |
approximately 1,500 pounds
|
| gptkbp:bfsParent |
gptkb:M1_Abrams_Tank
gptkb:M1_Abrams_tank |
| gptkbp:bfsLayer |
5
|