Re.2005 Sagittario
| GENERAL DATA | |||
| Other Designation(s) | - |
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| Type |
Fighter |
Crew | 1 |
| Manufacturer(s) | Reggiane |
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| Production | 48 (September 1942 – May
1944) |
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| Prototype first flight | 9 May 1942 |
Introduction | April/May 1943 |
| DIMENSIONS | |||
| Length | 8.73 m |
Empty Weight | 2600 kg |
| Wingspan | 11 m |
Loaded Weight | 3574 kg |
| Height | 3.15 m |
Max takeoff weight | 3610 kg |
| Wing area | 20.4 m² |
Wing loading | maximum 177 kg/m² |
| ARMAMENT | ||||
| Main Gun | Propeller
hub |
1 × 20 mm MG 151 cannon |
Ammunition Carried |
1 x 150 |
Wings |
2 × 20 mm MG 151 cannon |
2 x 200 |
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| Secondary Guns | Upper Cowling |
2 × 12.7 mm (.5 in) Breda-SAFAT MG |
Ammunition Carried | 2 x 350 |
| Bombs | Underfuselage (non standard)
hardpoint: 1000 kg bomb - Hardpoints on wings:
2 x 160 kg bombs |
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| POWERPLANT | |||
| Engine | 1 ×
Fiat R.A. 1050 RC 58 Tifone (license built DB 605A-1) |
Type & Displacement | liquid-cooled supercharged inverted
V-12 , 35.7 L |
| Horsepower (maximum) | 1475 hp |
Power/Weight Ratio | 412.70 hp / ton * |
| Fuel Capacity | 525 l L +
300 L drop tank ** and or not 2 × 150 L drop tanks ***
|
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(*) with the loaded weight, (**) Underfuselage, (***) Underwings
| PERFORMANCES | |||
| Maximum Speed | 628 km/h
at 6950 m |
Cruise Speed | 515 km/h |
| Stall Speed * | 155 km/h |
Service Ceiling | 11500 m |
| Rate of Climb | 20 m/s |
Range | 980 km, 1130 km**, 1270 km *** |
(*) vitesse de décrochage, (**) w/ 300 L drop tank, (***) w/ 300 L + 2 × 150 L drop tanks
| Sources | |||
| Wikipédia | - | - |
|
Drawings |
