Caratteristiche - Reggiane fighters
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Aircraft > RE2002
TECHNICAL DATA RE 2002
RE 2002 | |
First flight | October 1940 |
Units produced | 251 |
Units survived | 1 MM.8669 partly restored (Vigna di Valle) 1 MM.8700 fuselage (Limoges, F) 1 underwater aircraft (Corfu, GR) 1 set of relics (Ognina Cape) |
| Engine | Piaggio P.XIX RC45 "Turbine" |
Power | 1160 HP at 4500m |
Wingspan | 11 m |
| Length | 8.165 m |
Height | 3.15 m |
Wing area | 20.4 m2 |
Wing loading | 158 kg/m2 |
Loaded weight | 3240 kg |
Empty weight | 2390 kg |
Useful load | 850 kg |
Top speed | 530 km/h at 5500 m |
Min. speed | 120 km/h |
| Ceiling | 10500 m |
| Range | 1100 km |
| Armament | 2x SAFAT 12.7 mm, 2x SAFAT 7.7 mm |
The variant RE 2002 bis was prepared but not flown.
It was a RE 2002 with the wing of a RE 2005 but without radiators.
Performance as follows, according to Mr. Govi:
It was a RE 2002 with the wing of a RE 2005 but without radiators.
Performance as follows, according to Mr. Govi:
RE 2002 series | RE 2002 bis | |
| Wing | RE 2002 | RE 2005 |
| Vmax | 530 km/h @5500m | 580 km/h |
