Honeywell AGT1500 turbine engine
GPTKB entity
Statements (65)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:military_vehicles
|
| gptkbp:average_temperature |
up to 1,500 degrees Fahrenheit
|
| gptkbp:combustor_type |
annular combustion chamber
|
| gptkbp:compressor_type |
axial compressor
10 stages |
| gptkbp:configuration |
single spool
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control advanced control system |
| gptkbp:cooling_air_flow |
high airflow
|
| gptkbp:cooling_system |
air
air-cooled forced air cooling |
| gptkbp:design_purpose |
military applications
|
| gptkbp:emissions_standard |
meets military standards
|
| gptkbp:engine |
compact design
incorporates advanced technology comprehensive documentation available supported by extensive logistics developed for the U. S. Army quick start capability capable of upgrades for future needs used in various military platforms |
| gptkbp:engine_adaptability |
adaptable to various platforms
|
| gptkbp:engine_configuration |
modular design
meets stringent military specifications |
| gptkbp:engine_power |
high performance ratings
proven reliability in field use |
| gptkbp:engine_safety |
high safety standards
|
| gptkbp:engine_type |
gptkb:turbofan_engine
|
| gptkbp:first_introduced |
gptkb:1980
|
| gptkbp:fuel_capacity |
approximately 2 feet
approximately 1.5 feet approximately 4.5 feet |
| gptkbp:fuel_economy |
high efficiency
0.5 lb/hp/hr |
| gptkbp:fuel_type |
gptkb:JP-8
dual fuel system |
| gptkbp:gearbox |
integrated reduction gearbox
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell AGT1500 turbine engine
|
| gptkbp:ignition_system |
spark ignition
|
| gptkbp:investment |
high pressure
|
| gptkbp:is_tested_for |
extensive testing conducted
tested in advanced facilities |
| gptkbp:launch_window |
air start
|
| gptkbp:maintenance |
500 hours
designed for easy maintenance |
| gptkbp:manufacturer |
gptkb:Honeywell
|
| gptkbp:noise_level |
low noise emissions
|
| gptkbp:power_output |
1500 horsepower
|
| gptkbp:propulsion |
3,000 pounds
0.8 hp/lb |
| gptkbp:reliability |
high reliability
|
| gptkbp:service |
over 5,000 hours
|
| gptkbp:training |
training programs available for operators
|
| gptkbp:turbine_efficiency |
high thermal efficiency
|
| gptkbp:turbine_type |
single-stage turbine
nickel-based superalloy 1 stage |
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:M1_Abrams_tank
|
| gptkbp:weight |
approximately 1,200 pounds
|
| gptkbp:bfsParent |
gptkb:M2_A3_Bradley
|
| gptkbp:bfsLayer |
6
|