|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Gnome
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° C
|
|
gptkbp:certification
|
certified by EASA
|
|
gptkbp:controls
|
hydromechanical
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
Gnome et Rhône engineers
|
|
gptkbp:developer
|
1950s
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
compliant with ICAO standards
|
|
gptkbp:engine
|
gptkb:Gnome_Mk_101
horizontal
up to 5,000 hours
single engine assembly
|
|
gptkbp:engine_type
|
axial
free turbine
|
|
gptkbp:features
|
modular design
|
|
gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:fuel_capacity
|
0.5 m
1.5 m
0.7 m
high efficiency
0.5 kg/s
|
|
gptkbp:fuel_type
|
annular
kerosene
|
|
gptkbp:historical_significance
|
pioneering helicopter engine technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Gnome Mk 103
|
|
gptkbp:ignition_system
|
gptkb:park
|
|
gptkbp:legacy
|
influenced future turbine designs
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Gnome_et_Rhône
|
|
gptkbp:market_segment
|
gptkb:aircraft
|
|
gptkbp:max_speed
|
250 knots
|
|
gptkbp:noise_level
|
low noise
low vibration
|
|
gptkbp:notable_users
|
gptkb:starship
|
|
gptkbp:number_of_stages
|
two
|
|
gptkbp:operational_history
|
used in various military operations
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:power_output
|
1,100 shp
|
|
gptkbp:propulsion
|
3.67
turbo-shaft
1,100 lbf
|
|
gptkbp:retirement_year
|
phased out in the 1980s
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:setting
|
twin-spool
|
|
gptkbp:status
|
gptkb:archaeological_site
|
|
gptkbp:successor
|
gptkb:Gnome_Mk_104
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Westland_Wessex
|
|
gptkbp:weight
|
approximately 300 kg
|