| Manufacturer |
Ilyushin |
Antonov |
| Description |
The Ilyushin Il-46 was a jet-engined bomber produced in the USSR during 1951-2, as the result of a directive to redesign the Il-42 project (half the drawings had already been completed). |
The Antonov/Taqnia An-132 was an improved version of the Antonov An-32 twin-engined turboprop military transport aircraft that was under development jointly by Saudi Arabia and Ukraine. |
| First Flight |
1952-03-03 |
2017-03-31 |
| Designer |
Ilyushin |
Antonov |
| Length (m) |
25.325 |
24.53 |
| Height (m) |
|
8.8 |
| Max Seating |
|
75 |
| Max Speed (km/h) |
928 |
|
| Cruise Speed (km/h) |
|
550 |
| Max Ceiling (m) |
12700 |
9000 |
| Rate of Climb (m/s) |
12.25 |
|
| Armament |
3,000 kg of bombs (normal load); 6,000 kg of bombs (overload); 2 x 23 mm Nudelman-Rikhter NR-23 cannon fixed in the lower port fuselage; 2 x 23 mm Nudelman-Rikhter NR-23 cannon in an Il-K6 turret at the rear of the fuselage. |
|
| Capacity Description |
|
according to configuration, it can carry:; 9200 kg cargo.; 75 troops.; 27 stretchers. |
| National Origin |
Soviet Union |
Ukraine |
| Number Built |
1 |
1 |
| Powerplant Description |
2 × Lyul'ka AL-5, 49.05 kN thrust each |
2 × Pratt & Whitney Canada PW150A turboprops, 3781 kW (5071 hp) each |
| Status |
|
Cancelled |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Ilyushin_Il-46 |
en.wikipedia.org/wiki/Antonov/Taqnia_An-132 |
| Flat Wing Span (m) |
29 |
29.2 |
| Flat Wing Area (m²) |
105 |
|
| Aircraft Engine |
Lyulka AL-5 |
Pratt & Whitney Canada PW100 |
| Number of Engines |
2 |
2 |