Credit
3GO*CHN-405/mjordan_6 · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Z-10 · Length
Single source14.2 m (46 ft 7 in)[source]
S-92 · Length
Single sourceConfiguration
| Specification | Changhe Z-10 | Sikorsky S-92 |
|---|---|---|
| Type | Attack helicopter[source] | Medium-lift transport/utility helicopter[source] |
| Manufacturer | Changhe Aircraft Industries Corporation (CAIC)[source] | Sikorsky Aircraft[source] |
| Designer | 602nd Aircraft Design Institute Kamov Design Bureau[source] | — |
| Status | In service[source] | In service[source] |
| Primary user |
68 ft 6 in (20.88 m)[source]
S-92 · fuselage
Single source17 ft 3 in (5.26 m) fuselage[source]
S-92 · Range
Single source539 nmi (620 mi, 998 km)[source]
Z-10 · Combat range
Single source800–1,120 km (500–700 mi, 430–600 nmi)[source]
Z-10 · (2,400 ft/min) 23 mm PX-10 revolver cannon; WXG1006 electro-optical turret, pilot night vision system, a radar warning receiver (RWR), a missile approach warning system (MAWS) sensor, an IFF antenna, and armor plates can also be seen at the nose section
Single source12 m/s (2,400 ft/min) 23 mm PX-10 revolver cannon; WXG1006 electro-optical turret, pilot night vision system, a radar warning receiver (RWR), a missile approach warning system (MAWS) sensor, an IFF antenna, and armor plates can also be seen at the nose section[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
People's Liberation Army Ground Force Aviation People's Liberation Army Air Force Pakistan Army Aviation Corps[source] |
| — |
| Manufactured | 2003-present[source] | 1998–present[source] |
|---|
| Introduction date | 2009[source] | 2004[source] |
|---|
| First flight | 29 April 2003[source] | December 23, 1998[source] |
|---|
| Guns | 1x 23 mm (0.906 in) PX-10A revolver cannon[source] | — |
|---|
| Hardpoints | 4 with a capacity of 1,500 kg (3,307 lb) useful load , with provisions to carry combinations of: Rockets: on each hard point with 57 mm (2.244 in) rocket pod (19-tube) 70 mm (2.756 in) unguided rocket pod (7-tube) 70 mm (2.756 in) FS70 guided rocket pod (7-tube) with FS70A (GR-5) 70 mm (2.756 in) guided rocket or FS70B 70 mm (2.756 in) air burst fragmentation rocket 70 mm (2.756 in) unguided rocket pod (19-tube) 90 mm (3.543 in) rocket pod (7-tube) with FS90A 90 mm (3.543 in) guided rocket or Tianjian 90 mm (3.543 in) rockets Missiles: on each hard point with 4× HJ-8 , HJ-9 laser-guided air-to-surface missiles 4× AKD-10 (BA-7) laser-guided air-to-surface missiles 4× AKD-9 (BA-9) laser-guided air-to-surface missiles 4× AKD-21 (BA-21) millimetre-wave air-to-surface missiles 4× AG-300/M or AG-300/L laser-guided air-to-surface missiles 4× CM-502KG NLOS air-to-surface missiles 2× CM-501GA NLOS air-to-surface missiles 1× CM-501XA loitering munition 4× TY-90 air-to-air missiles Bombs: GB25 and GB50 guided bombs Other: 280kg drop tank[source] | — |
|---|
| g limits | +3[source] | — |
|---|
| Rockets | on each hard point with 57 mm (2.244 in) rocket pod (19-tube) 70 mm (2.756 in) unguided rocket pod (7-tube) 70 mm (2.756 in) FS70 guided rocket pod (7-tube) with FS70A (GR-5) 70 mm (2.756 in) guided rocket or FS70B 70 mm (2.756 in) air burst fragmentation rocket 70 mm (2.756 in) unguided rocket pod (19-tube) 90 mm (3.543 in) rocket pod (7-tube) with FS90A 90 mm (3.543 in) guided rocket or Tianjian 90 mm (3.543 in) rockets[source] | — |
|---|
| Missiles | on each hard point with 4× HJ-8 , HJ-9 laser-guided air-to-surface missiles 4× AKD-10 (BA-7) laser-guided air-to-surface missiles 4× AKD-9 (BA-9) laser-guided air-to-surface missiles 4× AKD-21 (BA-21) millimetre-wave air-to-surface missiles 4× AG-300/M or AG-300/L laser-guided air-to-surface missiles 4× CM-502KG NLOS air-to-surface missiles 2× CM-501GA NLOS air-to-surface missiles 1× CM-501XA loitering munition 4× TY-90 air-to-air missiles[source] | — |
|---|
| Bombs | GB25 and GB50 guided bombs[source] | — |
|---|
| Other | 280kg drop tank[source] | — |
|---|
| Country of origin | People's Republic of China[source] | — |
|---|
| National origin | — | United States[source] |
|---|
| Primary users | — | CHC Helicopter Petroleum Helicopters International Bristow Helicopters Cougar Helicopters[source] |
|---|
| Number built | — | at least 300[source] |
|---|
| Developed from | — | Sikorsky S-70[source] |
|---|
| Variants | — | Sikorsky CH-148 Cyclone Sikorsky VH-92[source] |
|---|
| Capacity | — | 19 passengers[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