Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crew |
1
|
| gptkbp:cruiseSpeed |
137 km/h
|
| gptkbp:emptyWeight |
430 kg
|
| gptkbp:engine |
Lycoming IVO-360-A1A
|
| gptkbp:engineType |
piston engine
|
| gptkbp:firstFlight |
1953
|
| gptkbp:height |
2.36 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Brantly B-2
|
| gptkbp:introduced |
1958
|
| gptkbp:length |
6.86 m
|
| gptkbp:mainRotorDiameter |
2
|
| gptkbp:manufacturer |
Brantly Helicopter Corporation
|
| gptkbp:maximumSpeed |
169 km/h
|
| gptkbp:maxTakeoffWeight |
726 kg
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:powerplant |
180 hp
|
| gptkbp:range |
322 km
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:seatingCapacity |
1
|
| gptkbp:serviceCeiling |
3,660 m
|
| gptkbp:status |
retired
|
| gptkbp:variant |
Brantly B-2A
Brantly B-2B |
| gptkbp:bfsParent |
gptkb:Lycoming_VO-435_engine
|
| gptkbp:bfsLayer |
7
|