Statements (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:Sultan
|
| gptkbp:application |
military helicopters
|
| gptkbp:compressionRatio |
8:1
|
| gptkbp:controls |
electronic control system
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:design |
turbo-shaft
|
| gptkbp:developer |
developed in the 1950s
|
| gptkbp:diameter |
approximately 14 in
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissionsStandard |
low emissions
|
| gptkbp:energyEfficiency |
high fuel efficiency
|
| gptkbp:engine |
lightweight
mounting frame |
| gptkbp:engineType |
two-stage turbine
single-stage centrifugal compressor |
| gptkbp:exhaustSystem |
axial exhaust
|
| gptkbp:firstFlight |
1955
|
| gptkbp:fuelCapacity |
0.5 lb/hp/hr
|
| gptkbp:fuelType |
Jet A
spark ignition hydromechanical fuel control |
| https://www.w3.org/2000/01/rdf-schema#label |
T53-L-703
|
| gptkbp:launched |
electric starter
|
| gptkbp:length |
approximately 40 in
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:noise_level |
low noise
|
| gptkbp:operationalStatus |
up to 1,000 °F
up to 30 psi |
| gptkbp:powerOutput |
1,500 shp
|
| gptkbp:propulsion |
1,100 to 1,800 shp
|
| gptkbp:related_engine |
Brayton_cycle
|
| gptkbp:reliability |
high reliability
|
| gptkbp:services |
20,000 ft
|
| gptkbp:setting |
free turbine
|
| gptkbp:successor |
T700 engine
|
| gptkbp:type |
turbo-shaft engine
|
| gptkbp:usedIn |
gptkb:Boeing_CH-47_Chinook
Bell UH-1 Iroquois |
| gptkbp:variant |
T53-L-703A
T53-L-703D T53-L-703B T53-L-703C T53-L-703E T53-L-703F T53-L-703G T53-L-703H T53-L-703I T53-L-703J |
| gptkbp:weight |
approximately 400 lb
|