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At a glance
Measured figures
H160 · Length
Single source13.96 m (45 ft 10 in)[source]
Length
Single sourceConfiguration
| Specification | Airbus Helicopters H160 | Mitsubishi RP-1 |
|---|---|---|
| Crew | 1/2[source] | — |
| Type | Medium utility helicopter[source] | Experimental twin-engined helicopter[source] |
| National origin | Multinational[source] | Japan[source] |
| Manufacturer | Airbus Helicopters[source] | Mitsubishi Heavy Industries[source] |
15.00 m (49 ft 2.5 in)[source]
H160 · Width
Single source3.54 m (11 ft 7 in)[source]
H160 · Main rotor diameter
Single source13.40 m (43.96 ft)[source]
Cruise; H160 · Cruise speed
Single source255 km/h (158 mph, 138 kn)[source]
H160 · Range
Single source880 km (550 mi, 475 nmi)[source]
H160 · with standard fuel tanks
Single source4 h 30 min with standard fuel tanks[source]
H160 · hover ceiling IGE
Single sourceH160 · Service ceiling
Single source6,096 m (20,000 ft) , 9,300 ft (2,835 m) hover ceiling IGE[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In production[source] | — |
|---|
| Manufactured | 2015–present[source] | — |
|---|
| Introduction date | 2021[source] | — |
|---|
| First flight | 13 June 2015[source] | 14 September 1994[source] |
|---|
| Capacity | 12[source] | — |
|---|
| Useful load | up to 2,000 kg (4,400 lb)[source] | — |
|---|
| Fuel capacity | 1,120 kg (2,470 lb)[source] | — |
|---|
| Main rotor area | 141 m 2 (1,520 sq ft)[source] | — |
|---|
| Never exceed speed | 315 km/h (196 mph, 170 kn)[source] | — |
|---|
| Disk loading | 42.9 kg/m 2 (8.8 lb/sq ft)[source] | — |
|---|
| Number built | — |
|---|
| Developed from | — | Sikorsky S-76[source] |
|---|
| Developed into | — | Mitsubishi MH2000[source] |
|---|