Properties (47)
Predicate | Object |
---|---|
gptkbp:instanceOf |
jet engine
|
gptkbp:application |
commercial aviation
|
gptkbp:controls |
hydromechanical
|
gptkbp:coolingSystem |
air-cooled
|
gptkbp:design_feature |
modular design
|
gptkbp:diameter |
3 ft 9 in
|
gptkbp:displacement |
significant in aviation history
|
gptkbp:emissionsStandard |
ICAO_Chapter_3
|
gptkbp:engine |
advanced materials
pylon-mounted factory assembled early turbojet technology influential in jet engine design used in early jetliners |
gptkbp:engineConfiguration |
single_spool
|
gptkbp:engineType |
axial
air start compatible with various aircraft CJ610-1 |
gptkbp:firstFlight |
1960
|
gptkbp:fuel_capacity |
high
0.85 lb/lbf/hr |
gptkbp:fuelType |
Jet A
annular |
gptkbp:hasArea |
static testing
FAA_certified |
https://www.w3.org/2000/01/rdf-schema#label |
General Electric CJ610
|
gptkbp:is_used_in |
gptkb:McDonnell_Douglas_DC-8
|
gptkbp:length |
12 ft 6 in
|
gptkbp:maintenance |
3,000 hours
|
gptkbp:manufacturer |
gptkb:General_Electric
|
gptkbp:market |
widely available
|
gptkbp:noise_level |
Stage 3 compliant
|
gptkbp:notableUsers |
gptkb:United_Airlines
|
gptkbp:number_of_stages |
8
|
gptkbp:operational_status |
military and civilian aircraft
|
gptkbp:performances |
high reliability
high thrust-to-weight ratio overhaul capability |
gptkbp:productionYears |
1950s to 1960s
|
gptkbp:propulsion |
18,500 lbf
5.78 |
gptkbp:services |
10,000 hours
|
gptkbp:successor |
gptkb:General_Electric_CF6
|
gptkbp:type |
turbojet engine
|
gptkbp:updates |
performance upgrades
|
gptkbp:weight |
3,200 lb
|