|
gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:aircraft
|
gptkb:Folland_Gnat
|
|
gptkbp:developer
|
gptkb:Rolls-Royce_Viper_family
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
Viper 601-22
Viper 601-23
Viper 601-24
Viper 601-25
Viper 601-26
Viper 601-27
Viper 601-28
Viper 601-29
Viper 601-30
Viper 601-31
Viper 601-32
Viper 601-33
Viper 601-34
Viper 601-35
Viper 601-36
Viper 601-37
Viper 601-38
Viper 601-39
Viper 601-40
Viper_632-41
|
|
gptkbp:firstFlight
|
1956
|
|
gptkbp:fuel_capacity
|
0.85 lb/lbf/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Viper 601
|
|
gptkbp:introduced
|
1956
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Buccaneer
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Navy
gptkb:Pakistan_Air_Force
|
|
gptkbp:operationalHistory
|
used in military aircraft
|
|
gptkbp:propulsion
|
5,000 lbf
|
|
gptkbp:related_engine
|
Rolls-Royce Viper 601-22
Brayton_cycle
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Viper_632
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:weight
|
1,200 lb
|