Statements (44)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:armament |
none
|
| gptkbp:crew |
1
|
| gptkbp:design |
gptkb:Bristol_Aeroplane_Company
|
| gptkbp:engine |
Bristol_Siddeley_A._1
|
| gptkbp:firstFlight |
1947
|
| gptkbp:height |
3.5 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bristol 171 Sycamore Mk 1
|
| gptkbp:length |
12.5 meters
|
| gptkbp:manufacturer |
gptkb:Bristol_Aeroplane_Company
|
| gptkbp:maxSpeed |
120 knots
|
| gptkbp:maxTakeoffWeight |
4,500 kg
|
| gptkbp:notableFeature |
low noise levels
easy maintenance good visibility used in reconnaissance missions large cabin space retractable landing gear used in military operations used in training missions adaptable for various missions used in civil aviation versatile operations two-blade rotor system good performance in cold climates good performance in hot climates high-mounted cockpit used in logistical support tandem_rotor_system |
| gptkbp:numberBuilt |
100
|
| gptkbp:passengerCapacity |
5
|
| gptkbp:primaryUser |
gptkb:British_Army
gptkb:Royal_Air_Force |
| gptkbp:range |
300 miles
|
| gptkbp:retirementYear |
1965
|
| gptkbp:role |
transport
utility helicopter medical evacuation search and rescue |
| gptkbp:rotorDiameter |
12.2 meters
|
| gptkbp:services |
1950
|
| gptkbp:successor |
gptkb:Bristol_192_Belvedere
|
| gptkbp:variant |
gptkb:Bristol_171_Sycamore_Mk_2
|
| gptkbp:weight |
2,500 kg
|