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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:military_aircraft
|
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gptkbp:average_temperature
|
1,000 ° C
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compression_ratio
|
6:1
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|
gptkbp:compressor_type
|
centrifugal compressor
|
|
gptkbp:control_system
|
hydraulic control
|
|
gptkbp:cooling_system
|
air-cooled
|
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gptkbp:country_of_origin
|
gptkb:Czechoslovakia
|
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gptkbp:design_date
|
1950s
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|
gptkbp:design_feature
|
lightweight materials
|
|
gptkbp:diameter
|
2.5 ft
|
|
gptkbp:emissions_standard
|
gptkb:CAA
|
|
gptkbp:engine
|
modular design
Brayton cycle
M601 D
|
|
gptkbp:engine_configuration
|
axial-flow
|
|
gptkbp:engine_power
|
1,500 hours
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1956
|
|
gptkbp:fuel_economy
|
high
0.85 lb/hp/hr
0.5 kg/s
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
gptkbp:history
|
developed from M601 A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Walter M601
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:legacy
|
influenced future designs
|
|
gptkbp:length
|
4.5 ft
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Walter_Engines
|
|
gptkbp:market_launch
|
gptkb:1958
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:notable_users
|
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:number_of_stages
|
gptkb:5
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:power_output
|
1,340 k W
|
|
gptkbp:propulsion
|
1.5
1,800 lbf
|
|
gptkbp:retirement_year
|
1970s
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Walter_M601_D
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Aero_L-29_Delfin
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:L-410_Turbolet
|
|
gptkbp:bfsLayer
|
6
|