P-61A Black Widow
| GENERAL DATA | |||
| Other Designation(s) | US:
P-61A |
||
| Type | Night
Fighter,Ground-Attack |
Crew | 2–3 (pilot, radar operator,
optional gunner) |
| Manufacturer(s) | Northrop |
||
| Production | 200 |
||
| First Flight | late 1943 |
Introduction | 1944 |
| DIMENSIONS | |||
| Empty Weight | 9510 kg |
Loaded Weight | 12519 kg |
| Max takeoff weight | 14697 kg |
Length | 15.11 m |
| Wingspan | 20.12 m |
Wing area | 61.53 m² |
| Height | 4.47 m |
Wing loading | 219 kg/m² |
| ARMAMENT | |||
| Main Guns | 4 × 20 mm (.79 in) Hispano
M2 cannon* |
Ammunition Carried | 4 x 200 |
| Secondary Guns | 4 × .50 in (12.7 mm) M2 Browning MG** |
Ammunition Carried | 560 |
| Other Armament | 4 x 726 kg bombs or 6 x 5 in (127
mm) HVAR unguided rockets could be carried under the wings. Some aircraft could also carry one 454 kg bomb under the fuselage. |
||
(*) Ventral position, (**) in remotely operated, full-traverse upper turret (first 37 only)
| POWERPLANT | |||
| Engine | 2 ×
Pratt & Whitney R-2800-65W * Double Wasp radial engines |
Type & Displacement | 18-cylinder air-cooled twin-row,
45.96 L |
| Horsepower (maximum) | 2
x 2250 hp at 3000 rpm |
Power/Weight Ratio | 359 hp / ton ** |
| Fuel Capacity |
2423 L (Up to four 625 L or 1173 L drop tanks under the wings)
|
||
(*) first 44 with Pratt & Whitney R-2800-45 (2000 hp), (**) with loaded weight
| PERFORMANCES | |||
| Maximum Speed | 594 km/h
at 6096 m |
Cruise Speed | ? km/h |
| Stall Speed * | ? km/h |
Service Ceiling | 10600 m |
| Rate of Climb | 12.9 m/s |
Range | 668 km (3060 km w/ 4 external fuel tanks) |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | Lemaire Soft | ||
Drawings |
File |
