Credit
Pritishp333 · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
HAL Rudralarger figure on 2 of 2
Mitsubishi RP-1larger figure on 0 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source15.87 m (52 ft 1 in)[source]
Length
Single sourceConfiguration
| Specification | HAL Rudra | Mitsubishi RP-1 |
|---|---|---|
| Crew | Two pilots[source] | — |
| Type | Armed helicopter[source] | Experimental twin-engined helicopter[source] |
| National origin | India[source] | Japan[source] |
| Manufacturer | Hindustan Aeronautics Limited[source] | Mitsubishi Heavy Industries[source] |
| Designer |
15.00 m (49 ft 2.5 in)[source]
Main rotor diameter
Single source13.2 m (43 ft 4 in)[source]
Service ceiling
Single source6,100 m (20,000 ft)[source]
2,033 ft/min
Single source10.33 m/s (2,033 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Rotary Wing Research and Design Centre[source] |
| — |
| Status | In service[source] | — |
|---|
| Primary users | Indian Army Indian Air Force[source] | — |
|---|
| Number built | 91[source] |
|---|
| Manufactured | 2007–present[source] | — |
|---|
| Introduction date | 2012[source] | — |
|---|
| First flight | 16 August 2007[source] | 14 September 1994[source] |
|---|
| Developed from | HAL Dhruv[source] | Sikorsky S-76[source] |
|---|
| Capacity | 12 passengers (14 passengers in high density seating)[source] | — |
|---|
| Fuel capacity | 1,055 kg (2,326 lb)[source] | — |
|---|
| Main rotor area | 136.85 m 2 (1,473.0 sq ft)[source] | — |
|---|
| Never exceed speed | 292 km/h (182 mph, 157 kn)[source] | — |
|---|
| Disk loading | 40.19 kg/m 2 (8.23 lb/sq ft)[source] | — |
|---|
| Developed into | — | Mitsubishi MH2000[source] |
|---|
| Reported operators |
| — |
|---|