Credit
Original uploader was User:Ahunt at en:wikipedia · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
F28F · Length
Single source29 ft 3 in (8.92 m)[source]
EC155 B1 · Length
Single sourceConfiguration
| Specification | Enstrom F-28 | Eurocopter EC155 |
|---|---|---|
| Crew | one[source] | 1 or 2 (pilots)[source] |
| Type | Light helicopter[source] | Passenger transport helicopter[source] |
| Manufacturer | Enstrom Helicopter Corporation[source] | Eurocopter Airbus Helicopters[source] |
| Manufactured | 1965-present[source] | 1997–present |
14.3 m (46 ft 11 in)[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]
EC155 B1 · 2 × Turbomeca Arriel 2C2 turboshaft engines, Take-off Power each
Single source2 × Turbomeca Arriel 2C2 turboshaft engines, Take-off Power, 697 kW (935 hp) each[source]
F28F · Endurance
Single source3 hr 30 min[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Introduction date | 1965[source] | March 1999[source] |
|---|
| Variants | Enstrom TH180 Spitfire Mark I[source] | — |
|---|
| Developed into | Enstrom 480[source] | Eurocopter X³ KAI LAH-1 Miron[source] |
|---|
| Capacity | two passengers[source] | 13 passengers or 2,301 kg (5,073 lb) payload[source] |
|---|
| Main rotor area | 804 sq ft (74.7 m 2 ) NACA 0013.5[source] | 124.7 m 2 (1,342 sq ft)[source] |
|---|
| Country of origin | Vereinigte Staaten[source]Country of design · Entwurfsland | — |
|---|
| National origin | — | Multinational[source] |
|---|
| Status | — | Active[source] |
|---|
| First flight | — | 17 June 1997[source] |
|---|
| Developed from | — | Eurocopter AS365 Dauphin[source] |
|---|
| Variant | — | KAI LCH[source] |
|---|
| Never exceed speed | — | 324 km/h (201 mph, 175 kn)[source] |
|---|
Maximum take-off; EC155 B1 · Max takeoff weight
Single source