Comparison of Kamov Ka-32A and Mil Mi-38 [S]ave
| Attribute |  Mil Mi-38 × |  Kamov Ka-32A × |
|---|---|---|
| General | ||
| Manufacturer | MIL Helicopters | Kamov |
| Model | Mil Mi-38 | Kamov Ka-32A |
| Country | Russia | Russia |
| Manufactured from (year) | 2003 | 1980 |
| Type | Large Helicopters | Large Helicopters |
| Icao | MI38 | KA32 |
| Performance | ||
| Engine | 2x Klimov TVA-3000 | 2x 2 X Klimov TV3-117V turboshafts |
| Power, hp (hp) | 2,465 | 2,190 |
| Avionics | Integrated Tactical System (FITS) | Israel Aerospace Industries. |
| Max cruise speed (km/h) | 300 | 230 |
| Travel range (km) | 883 | 982 |
| Fuel economy (km/l) | - | 0.342 |
| Service ceiling (m) | 6,492 | 5,000 |
| Rate of climb (m/sec) | 9.19 | 12.5 |
| Weights | ||
| Max take off weight (kg) | 15,600 | 12,700 |
| Max payload (kg) | 6,000 | 5,000 |
| Fuel tank capacity (l) | 3,937 | 2,650 |
| Baggage volume (m³) | 29.5 | 1 |
| Dimensions | ||
| Seats | 3 | 13 |
| Cabin height (m) | 1.8 | 1.24 |
| Cabin width (m) | 2.36 | 1.3 |
| Cabin length (m) | 7 | 4.52 |
| Exterior length (m) | 19.95 | 11.3 |
| Tail height (m) | 6.9 | 5.5 |
| Fuselage diameter (m) | 2.65 | 1.6 |
| Wing span (m) | 21.1 | 15.9 |
| Wing tips | No Winglets | No Winglets |
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