Credit
SDASM Archives · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Rockwell Aero Commander 500S · Length
Single source36 ft 9.75 in (11.22 m)[source]
Configuration
| Specification | Aero Commander 500 family | Antonov An-72 |
|---|---|---|
| Crew | Two[source] | five[source] |
| Type | Utility and business aircraft[source] | Transport aircraft[source] |
| National origin | United States[source] | Soviet Union[source] |
| Manufacturer | Aero Design and Engineering Company Aero Commander Rockwell-Standard Corporation North American Rockwell Rockwell International Gulfstream Aerospace[source] |
An-72 · Length
28.07 m (92 ft 1 in)[source]
Empty; Rockwell Aero Commander 500S · Empty weight
Single sourceMaximum take-off; Rockwell Aero Commander 500S · Max takeoff weight
Single source4,635 lb (2,102 kg)[source]
6,750 lb (3,062 kg)[source]
Empty; An-72 · Empty weight
Single sourceGross; An-72 · Gross weight
Single sourceCruise; Rockwell Aero Commander 500S · at 9,000 ft (2,750 m), 75% power, TAS
Single sourceMaximum; Rockwell Aero Commander 500S · at sea level ( TAS )
Single source215 mph (346 km/h, 187 kn) at sea level ( TAS )[source]
203 mph (326 km/h, 176 kn) at 9,000 ft (2,750 m), 75% power, TAS[source]
Maximum; An-72 · Maximum speed
Single source700 km/h (435 mph, 378 kn)[source]
Rockwell Aero Commander 500S · 2 × Lycoming IO-540 -E1B5 air-cooled flat-six piston engines each
Single source2 × Lycoming IO-540 -E1B5 air-cooled flat-six piston engines , 290 hp (216 kW) each[source]
An-72 · 2 × Lotarev D-36 series 1A Turbofan thrust each
Single source2 × Lotarev D-36 series 1A Turbofan, 63.9 kN (14,330 lbf) thrust each[source]
Rockwell Aero Commander 500S · 1,340 ft/min (
Single source1,340 ft/min (6.8 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Antonov[source] |
| Status | Active[source] | In service[source] |
|---|
| Number built | ~2,902 (1951 piston-engined, 951 turboprops)[source] | 133[source] |
|---|
| Manufactured | 1951–1986[source] | 1977–2002[source] |
|---|
| Introduction date | October 1952[source] | — |
|---|
| First flight | 23 April 1948 (Model L3085)[source] | 31 August 1977 ( 1977-08-31 )[source] |
|---|
| Developed into | IAI Westwind[source] | Antonov An-71 Antonov An-74[source] |
|---|
| Capacity | four passengers[source] | up to 52 passengers or 10 tonnes of cargo[source] |
|---|
| Aspect ratio | 9.45:1[source] | — |
|---|
| Airfoil | NACA 23012 modified[source] | — |
|---|
| Stall speed | 68 mph (109 km/h, 59 kn) flaps and landing gear down, CAS[source] | — |
|---|
| Minimum control speed | 75 mph (121 km/h, 65 kn)[source] | — |
|---|
| Primary users | — | Russian Aerospace Forces Russian Navy Angolan Air Force Soviet Air Force (historical)[source] |
|---|
| Reported operators | — |
|
|---|