Credit
Vitaly V. Kuzmin · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
An-70 · Length
Single source40.73 m (133 ft 8 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Antonov An-70 | Cirrus SR20 |
|---|---|---|
| Type | Military transport aircraft[source] | Light aircraft[source] |
| National origin | Soviet Union Ukraine[source] | United States[source] |
| Designer | Antonov Design Bureau[source] | — |
| Built by | Antonov Serial Production Plant[source] | — |
| Status | Completed state tests, open for production[source] |
26 ft 0 in (7.92 m)[source]
Cruise; An-70 · at 9,100–11,000 m (29,900–36,100 ft)
Single sourceMaximum; An-70 · Maximum speed
Single source780 km/h (480 mph, 420 kn)[source]
750 km/h (470 mph, 400 kn) at 9,100–11,000 m (29,900–36,100 ft)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
An-70 · runway
Single sourceAn-70 · with 47,000 kg (103,617 lb) payload from
Single source1,350 km (840 mi, 730 nmi) with 47,000 kg (103,617 lb) payload from 1,800 m (5,900 ft) runway[source]
An-70 · 4 × Progress D-27 propfan each
Single source4 × Progress D-27 propfan , 10,350 kW (13,880 hp) each[source]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Primary user | Ukrainian Air Force[source] | — |
|---|
| Number built | 2 prototypes[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1991–1996 2012–2015[source] | 1999–present[source] |
|---|
| First flight | 16 December 1994[source] | 21 March 1995[source] |
|---|
| Capacity | 300 troops or 206 stretcher cases / 47,000 kg (103,617 lb) max payload[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Airfoil | TsAGI P-202[source] | — |
|---|
| Propellers | 14-bladed Aerosyla Stupino SV-27, 4.5 m (14 ft 9 in) diameter contra-rotating propeller (8-bladed forward; 6-bladed rear)[source] | 3-bladed[source] |
|---|
| Stall speed | 113 km/h (70 mph, 61 kn)[source] | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| Power/mass | 0.316 kW/kg (0.192 hp/lb) max[source] | — |
|---|
| Take-off field length | 1,800 m (5,900 ft)[source] | — |
|---|
| Landing field length | 2,000 m (6,600 ft)[source] | — |
|---|
| Take-off run STOL 30,000 kg (66,139 lb) payload | 600 m (2,000 ft)[source] | — |
|---|
| Take-off run STOL 35,000 kg (77,162 lb) payload | 915 m (3,000 ft)[source] | — |
|---|
| Manufacturer | Kyiv Aircraft Production Plant[source] | Cirrus Aircraft[source] |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|