|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:T-33_C
gptkb:T-33_E
gptkb:T-33_Q
gptkb:T-33_V
|
|
gptkbp:aircraft_operated
|
gptkb:Mc_Donnell_F2_H_Banshee
gptkb:Lockheed_F-94_Starfire
gptkb:North_American_F-86_Sabre
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
high temperature
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:controls
|
manual control
|
|
gptkbp:cooling_system
|
air-cooled
intercooling
|
|
gptkbp:design
|
axial-flow design
|
|
gptkbp:developer
|
J42 turbojet
|
|
gptkbp:diameter
|
3 ft
|
|
gptkbp:emissions_standard
|
straight exhaust
subsonic intake
moderate emissions
|
|
gptkbp:engine
|
high performance
modular design
Brayton cycle
compact design
2000 hours
wing-mounted
air start
turbojet configuration
influenced future turbojet designs
major overhaul required every 1000 hours
early turbojet innovations
|
|
gptkbp:engine_type
|
axial
single-engine
single spool
constant pressure cycle
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_capacity
|
moderate efficiency
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
annular
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
J33 turbojet
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:legal_issue
|
jet propulsion
|
|
gptkbp:length
|
12 ft
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
0.9 Mach
|
|
gptkbp:noise_level
|
high noise
|
|
gptkbp:operational_range
|
high subsonic to low supersonic
|
|
gptkbp:propulsion
|
4.17
no thrust vectoring
5000 lbf
4.2 lbf/lb
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
J57 turbojet
|
|
gptkbp:weight
|
1200 lb
|