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gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
|
gptkb:F2H_Banshee
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gptkbp:application
|
military aircraft
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gptkbp:climate
|
1500 °F
|
|
gptkbp:controls
|
hydromechanical
|
|
gptkbp:coolingSystem
|
air-cooled
air-cooled design
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gptkbp:design
|
Axial-flow
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gptkbp:developer
|
gptkb:Allison_J35
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gptkbp:diameter
|
3 ft 4 in
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|
gptkbp:emissionsStandard
|
Stage 3
|
|
gptkbp:engine
|
gptkb:Allison_J35_series
pylon-mounted
1950s technology
J35-1
|
|
gptkbp:engineConfiguration
|
single-spool
|
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gptkbp:engineType
|
2
8
afterburning turbojet
air start
J35-A-1
|
|
gptkbp:firstFlight
|
1949
|
|
gptkbp:fuel_capacity
|
0.8 lb/hp/hr
1000 lb/hr
|
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gptkbp:fuelType
|
Jet A
spark plug
can-type
|
|
gptkbp:hasArea
|
extensive ground testing
FAA_certified.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Allison J35-A-1
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Allison_Engine_Company
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:notableUsers
|
gptkb:McDonnell_F2H_Banshee
|
|
gptkbp:operationalHistory
|
used in several aircraft
|
|
gptkbp:performances
|
high reliability
2000 hours
high thrust-to-weight ratio
1,500 hours
every 1,000 hours
moderate efficiency
|
|
gptkbp:propulsion
|
0.24
4.17
5,000 lbf
5000 lbf
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Allison_J71
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:weight
|
1200 lb
|