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ForceTally · AI-generated illustration · Not a photograph · AI-generated · OpenAI output terms · Source ↗ · Modified
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At a glance
HESA Shahed 274larger figure on 0 of 2
Mitsubishi RP-1larger figure on 2 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source9 m (29 ft 6 in)[source]
Length
Single sourceConfiguration
| Specification | HESA Shahed 274 | Mitsubishi RP-1 |
|---|---|---|
| Type | Light utility helicopter[source] | Experimental twin-engined helicopter[source] |
| Manufacturer | Iran Aircraft Manufacturing Industrial Company[source] | Mitsubishi Heavy Industries[source] |
| Designer | Institute of Industrial Research and Development of the IRGC[source] | — |
| Status | Unknown[source] | — |
| Primary user | Islamic Revolutionary Guard Corps |
15.00 m (49 ft 2.5 in)[source]
Main rotor diameter
Single source10 m (32 ft 10 in)[source]
Maximum; Maximum speed
Single source180 km/h (112 mph, 97 kn)[source]
Service ceiling
Single source5,200 m (17,100 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | At least 3[source] |
|---|
| Introduction date | 30 December 2000[source] | — |
|---|
| First flight | 1997[source] | 14 September 1994[source] |
|---|
| Capacity | 5 (including pilot)[source] | — |
|---|
| Propellers | 2-bladed main and tail[source] | — |
|---|
| National origin | Iran[source] | Japan[source] |
|---|
| Developed from | — | Sikorsky S-76[source] |
|---|
| Developed into | — | Mitsubishi MH2000[source] |
|---|