Credit
3GO*CHN-405/mjordan_6 · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Z-10 · Length
Single source14.2 m (46 ft 7 in)[source]
F28F · Length
Single sourceConfiguration
| Specification | Changhe Z-10 | Enstrom F-28 |
|---|---|---|
| Type | Attack helicopter[source] | Light helicopter[source] |
| Manufacturer | Changhe Aircraft Industries Corporation (CAIC)[source] | Enstrom Helicopter Corporation[source] |
| Designer | 602nd Aircraft Design Institute Kamov Design Bureau[source] | — |
| Status | In service[source] | — |
| Primary user | People's Liberation Army Ground Force Aviation People's Liberation Army Air Force Pakistan Army Aviation Corps |
29 ft 3 in (8.92 m)[source]
F28F · Range
Single source241 nmi (277 mi, 446 km)[source]
Z-10 · Combat range
Single source800–1,120 km (500–700 mi, 430–600 nmi)[source]
Z-10 · 2 × WZ-9C turboshaft engines each
Single source2 × WZ-9C turboshaft engines, 1,200 kW (1,600 hp) each[source]
F28F · 1 × Lycoming HIO-360-F1AD four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine
Single source1 × Lycoming HIO-360-F1AD four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine, 225 hp (168 kW)[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]
F28F · 1,450 ft/min (
Single source1,450 ft/min (7.4 m/s)[source]
F28F · Endurance
Single source3 hr 30 min[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Manufactured | 2003-present[source] | 1965-present[source] |
|---|
| Introduction date | 2009[source] | 1965[source] |
|---|
| First flight | 29 April 2003[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] | Vereinigte Staaten[source]Country of design · Entwurfsland |
|---|
| Variants | — | Enstrom TH180 Spitfire Mark I[source] |
|---|
| Developed into | — | Enstrom 480[source] |
|---|
| Capacity | — | two passengers[source] |
|---|
| Main rotor area | — | 804 sq ft (74.7 m 2 ) NACA 0013.5[source] |
|---|