Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:capacity |
6 passengers
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crew |
2
|
| gptkbp:engine |
gptkb:Continental_R-975-46
|
| gptkbp:enginePower |
550 hp
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
March 1952
|
| gptkbp:height |
12 ft 9 in
|
| gptkbp:introduced |
1953
|
| gptkbp:length |
41 ft 4 in
|
| gptkbp:mainRotorDiameter |
44 ft
|
| gptkbp:manufacturer |
gptkb:Piasecki_Helicopter
|
| gptkbp:maximumSpeed |
96 mph
|
| gptkbp:NATOReportingName |
gptkb:Hound
|
| gptkbp:notableFeature |
tandem rotor design
|
| gptkbp:numberBuilt |
339
|
| gptkbp:otherName |
gptkb:HUP_Retriever
|
| gptkbp:range |
215 mi
|
| gptkbp:retired |
1964
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:serviceCeiling |
10,000 ft
|
| gptkbp:usedBy |
gptkb:United_States_Army
gptkb:United_States_Navy gptkb:Royal_Canadian_Navy |
| gptkbp:usedFor |
anti-submarine warfare
rescue missions utility transport |
| gptkbp:bfsParent |
gptkb:Operation_Highjump_(1946–1947)
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Piasecki H-25 Army Mule
|