I.A.R. 81C
GENERAL DATA |
- |
Fighter, Dive Bomber, Strike Aircraft
|
1 |
Caproni-Vizzola
SA |
170 IAR 80 and 176 IAR 81 on September
30, 1944 |
12 April 1939 (IAR 80) |
February 1941 |
Variants |
Base production model, 4 x 7.92 mm MG (170 examples
produced) |
6 x 7.92 mm MG, improved armor for the pilot |
Lenghtened wings, improved radio eqipment, provision
for underwing bombs or fuel tanks, 13.2 mm MG. |
Redisigned I.A.R. 80A models to I.A.R. 81C weapons standard
of 4 x 7.92 mm MG and 2 x 20 mm Cannons. |
Two-Seat Trainer Conversion Model |
Fighter-Bomber, Dive-Bomber Model (176 examples produced) |
Fighter-Model, 13.2 mm MG. |
Redisigned wings to incorporate MG FF/M cannons, self-sealing
fuel tanks and improved armor protection for the pilot |
Fitted with Mauser MG 151/20 guns |
Redisigned I.A.R. 80B models to I.A.R. 81C weapons standard
of 4 x 7.92 mm MG and 2 x 20 mm Cannons. |
DIMENSIONS |
8.97 m |
1617 kg |
11 m |
2200 kg |
3.60 m |
3030 kg |
17 m² |
132.35 kg/m² |
ARMAMENT |
2 × 20 mm (0.787 in) MG 151/20
cannon * |
2 x ? |
2 x 7.92 mm (0.312 in) FN-Browning * |
2 x ? |
one 250 kg SC250 bomb under the
fuselage and/or 2 × 50 kg SC50 bombs under the wings |
(*) mounted in the inner portion of the
wing
POWERPLANT |
1 ×
IAR K14-IV C32 1000A |
R14-cylinder two-row
air-cooled, 38.673 L |
1025 hp |
465.91 hp / ton * |
555 L + 2
x 100 L drop fuel tanks
|
(*) with the loaded weight
PERFORMANCES |
524 km/h
at 5350m |
? km/h |
? km/h |
10000 m |
? m/s |
730 km, 1300 km (w/ extra fuel tanks) |
(*) vitesse de décrochage
|