Credit
Original uploader was User:Ahunt at en:wikipedia · Public domain · Resized · Public domain · Source ↗ · Modified
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At a glance
Measured figures
F28F · Length
Single source29 ft 3 in (8.92 m)[source]
overall
Single sourceConfiguration
| Specification | Enstrom F-28 | Kamov Ka-60 |
|---|---|---|
| Crew | one[source] | 1 or 2[source] |
| Type | Light helicopter[source] | Transport/utility helicopter[source] |
| Manufacturer | Enstrom Helicopter Corporation[source] | Kamov[source] |
| Manufactured | 1965-present[source] | — |
| Introduction date | 1965 |
15.6 m (51 ft 2 in) overall[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]
2 × Turbomeca Ardiden 3G turboshaft (1,776 shp) each
Single source2 × Turbomeca Ardiden 3G turboshaft , 1,324 kW (1,776 shp) each[source]
F28F · Endurance
Single source3 hr 30 min[source]
F28F · 1,450 ft/min (
Single source1,450 ft/min (7.4 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Variants | Enstrom TH180 Spitfire Mark I[source] | — |
|---|
| Developed into | Enstrom 480[source] | — |
|---|
| Capacity | two passengers[source] | 12–15 passengers ( Ka-62 ) 14 infantry troops or 6 stretchers Internal 2,000 kg (4,409 lb) External 2,500 kg (5,512 lb)[source] |
|---|
| Main rotor area | 804 sq ft (74.7 m 2 ) NACA 0013.5[source] | 143.1 m 2 (1,540 sq ft)[source] |
|---|
| Country of origin | Vereinigte Staaten[source]Country of design · Entwurfsland | — |
|---|
| National origin | — | Russia[source] |
|---|
| Number built | — |
|---|
| First flight | — | 24 December 1998[source] |
|---|
| Hover ceiling | — | 3,300 m (10,827 ft)[source] |
|---|