Test_volo - Reggiane fighters
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Aircraft > RE2001
FLIGHT TESTS
11.1941 Report AR-60
(These features are draft, as currently being checked by technical authorities)
| Top speed at 5470 m | 560 km/h |
| Top speed at 0 m | 435 km/h |
| Min. speed with extended flaps | 110 km/h |
| Climb to 4000 m | 4'15" |
| Climb to 6000 m | 6'50" |
| Ceiling | 11800 m |
| Take off run | 168 m |
| Land run | 255 m |
| Range with standard fuel load (316 kg) at 4800 m and 469 km/h | 2h |
| Empty weight | 2388 kg |
| Useful weight | 782 kg |
| Total weight | 3170 kg |
| Wing load | 155 kg/m2 |
| Load/HP ratio at 4000 m | 2,880 kg |
| Max load factor | 13 |
6.9.40-8.10.40 Flight test performed in Guidonia on a prototype RE 2001 (from "comunicaz della D.G.C.A. - Relazione di Guidonia 6.9.40-8.10.40")
| Aircraft | RE2001 prototype - MM409 |
| Engine | DB601Aa |
| Power | 1000 HP @ 4500 m |
Wingspan | 11 m |
| Length | 8.36 m |
| Height | 3.15 m |
Wing area | 20.4 m2 |
Wing loading | 133.7 kg/m2 |
Loaded weight | 2728 kg |
Empty weight | 2118 kg |
Useful weight | 610 kg |
Top speed | 563 km/h @ 5470 m |
Cruise speed | 450 km/h |
Min. speed | 119.5 km/h |
| Ceiling | 11800 m |
| Range | 820 km |
Climb to 1000 m | 41" |
Climb to 2000 m | 1'27" |
Climb to 3000 m | 2'19" |
Climb to 4000 m | 3'30" |
Climb to 5000 m | 4'32" |
Climb to 6000 m | 5'43" |
Take off run | 168 m |
Land run | 255 m |
| Armament | 2x SAFAT da 12.7 mm |
