Sikorsky H-53 Sea Stallion
Aircraft of the U.S. Marines Corps
Entwicklung
Ordered
Bestellt
Versionen
Two prototypes with two 2,850 shp T64-GE-3 engines.
Initial production for USMC, 139 built
CH-53A re-engined with two 3,925 shp T64-GE-413 engines as Airborne mine countermeasures versions for the US Navy, 15 conversion.
CH-53A with improved transmission, larger cabin for 55 troops and automatic rotor blade folding for the US Marine Corps, 126 built.
United States Navy mine countermeasures version of the CH-53D
Two CH-53Ds for USMC VIP transport
Super Stallion
Three engined version of the CH-53D, 177 build
Sea Dragon U.S.s Navy mine countermeasures version of the CH-53E
Einsatzgeschichte
O
G
Zeichnungen
| Specifications |
CH-53D |
CH-53E |
|
|
Rotor diameter |
Rotordurchmesser |
22.01 m |
24.00 m |
|
Length |
Länge |
26.97 m |
30.20 m |
|
Height |
Höhe |
7.60 m |
8.46 m |
|
Engine |
Motor |
2× General Electric T64-GE-413 turboshaft, 3,925 shp each |
3× General Electric T64-GE-416/416A turboshaft, 4,380 shp each |
|
Maximum speed |
Höchstgeschwindigkeit |
315 km/h |
315 km/h |
|
Empty weight |
Leergewicht |
10,740 kg |
15,071 kg |
|
Loaded weight |
Startgewicht |
19,100 kg |
33,300 kg |
|
Climb Rate |
Steigrate |
12.5 m/s |
13 m/s |
|
Service ceiling |
Gipfelhöhe |
5,106 m |
5,640 m |
|
Range |
Reichweite |
1,000 km |
1,000 km |
|
Armament |
Bewaffnung |
3× 12.7 machine guns |
3× 12.7 machine guns |
| Serials, Sikorsky H-53 Sea Stallion | ||
|
YCH-53A |
151613 - 151614 |
2 |
|
CH-53A |
151686 - 151701 |
16 |
|
CH-53A |
152392 - 152415 |
|
|
CH-53A |
153274 - 153313 |
|
|
CH-53A |
153705 - 153739 |
|
|
CH-53A |
154863 - 154884 |
|
|
CH-53G |
154885 - 154886 |
|
|
CH-53A |
154887 - 154888 |
|
|
CH-53D |
156654 - 156677 |
|
|
CH-53D |
156951 - 156970 |
|
|
CH-53D |
157127 - 157176 |
|
|
CH-53D |
157727 - 157756 |
|
|
CH-53D |
157930 - 157931 |
|
|
CH-53D |
|
|
|
Total |
1 |
|
