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At a glance
Measured figures
HH-60G · Length
Single source64 ft 10 in (19.76 m)[source]
S-92 · Length
Single sourceConfiguration
| Specification | Sikorsky HH-60 Pave Hawk | Sikorsky S-92 |
|---|---|---|
| Type | Combat search and rescue helicopter[source] | Medium-lift transport/utility helicopter[source] |
| Manufacturer | Sikorsky Aircraft[source] | Sikorsky Aircraft[source] |
| Status | In service[source] | In service[source] |
| Primary users | United States Air Force Republic of Korea Air Force[source] | CHC Helicopter Petroleum Helicopters International Bristow Helicopters Cougar Helicopters |
68 ft 6 in (20.88 m)[source]
S-92 · fuselage
Single source17 ft 3 in (5.26 m) fuselage[source]
HH-60G · 2 × General Electric T700-GE-700 / -701C turboshaft engines, 1,940 shp ( ) each
Single source2 × General Electric T700-GE-700 / -701C turboshaft engines, 1,940 shp (1,450 kW) each[source]
S-92 · 2 × General Electric CT7-8A turboshaft engines, 2,520 shp ( ) each
Single source2 × General Electric CT7-8A turboshaft engines, 2,520 shp (1,880 kW) each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 112 (HH-60G Pave Hawk)[source] | at least 300[source] |
|---|
| Introduction date | 1982[source] | 2004[source] |
|---|
| Developed from | Sikorsky UH-60 Black Hawk[source] | Sikorsky S-70[source] |
|---|
| Capacity | maximum crew 6 / 8 to 12 troops / litters or other cargo[source] | 19 passengers[source] |
|---|
| Country of origin | United States[source] | — |
|---|
| National origin | — | United States[source] |
|---|
| Manufactured | — | 1998–present[source] |
|---|
| First flight | — | December 23, 1998[source] |
|---|
| Variants | — | Sikorsky CH-148 Cyclone Sikorsky VH-92[source] |
|---|
| Cabin dimensions | — | 20 ft (6 m) long by 6.6 ft (2 m) tall[source] |
|---|
| Main rotor area | — | 2,492.3 sq ft (231.54 m 2 )[source] |
|---|
| Blade section | — | - root: Sikorsky SC2110; tip: Sikorsky SSC-A09[source] |
|---|
| Disk loading | — | 9.8 lb/sq ft (48 kg/m 2 )[source] |
|---|
| Power/mass | — | 0.23 hp/lb (0.38 kW/kg)[source] |
|---|
Maximum take-off; S-92 · Max takeoff weight
Single source