Statements (49)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:armament |
machine guns
|
| gptkbp:capacity |
up to 55 troops
|
| gptkbp:crew |
2
|
| gptkbp:design |
twin-engine
heavy-lift |
| gptkbp:engine |
T64-GE-416 turboshaft
|
| gptkbp:firstFlight |
1964
|
| gptkbp:height |
26 ft 2 in (7.98 m)
|
| https://www.w3.org/2000/01/rdf-schema#label |
Sikorsky CH-53 family
|
| gptkbp:introduced |
1966
|
| gptkbp:length |
99 ft 0 in (30.18 m)
|
| gptkbp:manufacturer |
gptkb:Sikorsky_Aircraft_Corporation
|
| gptkbp:maxSpeed |
170 knots (196 mph; 315 km/h)
|
| gptkbp:notableFeature |
advanced avionics
multi-mission capabilities multi-role capabilities long-range missions combat search and rescue capabilities high survivability high payload capacity search and rescue capabilities high-altitude operations special operations capabilities support for amphibious operations external cargo hooks refueling capabilities transport of heavy equipment versatile operational roles heavy armor options three rotor blades |
| gptkbp:passengerCapacity |
up to 30,000 lb (13,600 kg)
|
| gptkbp:range |
600 nautical miles (690 mi; 1,110 km)
|
| gptkbp:retired |
in some air forces
|
| gptkbp:role |
transport helicopter
|
| gptkbp:services |
15,000 ft (4,600 m)
|
| gptkbp:successor |
gptkb:CH-53K_King_Stallion
|
| gptkbp:usedBy |
gptkb:Israeli_Air_Force
gptkb:Royal_Netherlands_Air_Force gptkb:Royal_Australian_Air_Force gptkb:United_States_Air_Force gptkb:German_Air_Force gptkb:United_States_Marine_Corps |
| gptkbp:variant |
CH-53E Super Stallion
MH-53 Pave Low CH-53A Sea Stallion CH-53D Sea Stallion |
| gptkbp:weight |
up to 73,000 lb (33,000 kg) max takeoff weight
|
| gptkbp:wingspan |
79 ft 0 in (24.08 m)
|