|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:application
|
military aircraft
civil aircraft
|
|
gptkbp:controls
|
hydraulic control system
|
|
gptkbp:coolingSystem
|
air-cooled
direct air cooling
|
|
gptkbp:diameter
|
2 ft 6 in
|
|
gptkbp:engineConfiguration
|
single_spool
|
|
gptkbp:engineType
|
axial compressor
air start
single-stage turbine
|
|
gptkbp:firstFlight
|
1951
|
|
gptkbp:fuelType
|
kerosene
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Viper family
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Harrier
BAC Strikemaster
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:notableUsers
|
gptkb:Singapore_Air_Force
gptkb:British_Aerospace
gptkb:Argentine_Air_Force
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:Pakistan_Air_Force
gptkb:South_African_Air_Force
gptkb:Malaysia_Air_Force
|
|
gptkbp:operational_status
|
attack aircraft
fighter aircraft
training aircraft
trainer aircraft
|
|
gptkbp:origin
|
gptkb:United_Kingdom
|
|
gptkbp:performances
|
modular design
|
|
gptkbp:propulsion
|
3,000 lbf
|
|
gptkbp:successor
|
Rolls-Royce Adour
|
|
gptkbp:team
|
gptkb:Rolls-Royce
|
|
gptkbp:type
|
turbojet engine
|
|
gptkbp:variant
|
gptkb:Viper_632
Viper 601
Viper 702
|
|
gptkbp:weight
|
1,200 lb
|