gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:armament
|
none
|
gptkbp:cockpit
|
two-seat cockpit
|
gptkbp:crew
|
1
|
gptkbp:engine
|
gptkb:Bristol_Siddeley_Viper
|
gptkbp:firstFlight
|
1947
|
gptkbp:firstGeneration
|
gptkb:British_Army
gptkb:British_Army_Air_Corps
|
gptkbp:fuelCapacity
|
500 liters
|
gptkbp:headlights
|
two-bladed tail rotor
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol 171 Sycamore Mk 2
|
gptkbp:introduced
|
1950
|
gptkbp:landingGear
|
skid landing gear
|
gptkbp:length
|
12.5 m
|
gptkbp:manufacturer
|
gptkb:Bristol_Aeroplane_Company
|
gptkbp:maxSpeed
|
150 km/h
|
gptkbp:maxTakeoffWeight
|
3,600 kg
|
gptkbp:notableFeature
|
piston engine
low noise levels
easy maintenance
good visibility
two-bladed main rotor
large cabin space
retractable landing gear
high-mounted rotor system
tailwheel configuration
versatile operations
good performance at high altitudes
good performance in cold climates
good performance in hot climates
|
gptkbp:numberBuilt
|
100
|
gptkbp:passengerCapacity
|
up to 5
|
gptkbp:powers
|
420 shp
|
gptkbp:range
|
500 km
|
gptkbp:retired
|
1960s
|
gptkbp:role
|
training
transport
utility helicopter
search and rescue
air ambulance
|
gptkbp:rotorDiameter
|
12.2 m
|
gptkbp:services
|
3,000 m
|
gptkbp:successor
|
gptkb:Bristol_192_Belvedere
|
gptkbp:usedBy
|
gptkb:Royal_Air_Force
gptkb:Royal_Navy
|
gptkbp:variant
|
gptkb:Bristol_171_Sycamore_Mk_1
Bristol_171_Sycamore_Mk_3
|
gptkbp:weight
|
2,500 kg
|