Northrop P-61 Black Widow
The Northrop P-61 Black Widow was the first operational U.S. warplane explicitly designed to be a night fighter.
Northrop P-61 Black Widow - WW2 American Aircraft & Warplanes

Time Period: World War II
Country of Origin: United States
Type: Fighter Aircraft (Light Fighter)
Manufacturer: Northrop Corporation

Northrop P-61 Aircraft Overview

The Northrop P-61 Black Widow was a night fighter aircraft developed by Northrop Corporation during World War II. It was the first operational U.S. military aircraft designed specifically for the night-fighting role.

The P-61 was a twin-engine, twin-boom aircraft with a crew of three. It was armed with four 20mm cannons and four .50 caliber machine guns and had a radar system that allowed it to detect and engage enemy aircraft at night.

The P-61 entered service with the United States Army Air Forces (USAAF) in 1944 and saw combat in both the European and Pacific theaters of the war. It was primarily used for night interception and ground attack missions, and was particularly effective at destroying enemy bombers.

In addition to its role as a night fighter, the P-61 was also used as a transport aircraft, with some versions modified to carry personnel or cargo.

Despite its effectiveness, the P-61 was retired from service shortly after the end of World War II, as advances in radar technology led to the development of more advanced night fighters. However, a few P-61s were used by the United States Air Force for reconnaissance and training missions until the early 1950s.

Today, several P-61s are preserved in museums and private collections around the world, serving as a reminder of this important aircraft’s role in World War II.

Northrop P-61 Specifications

  • Crew: 2–3 (pilot, radar operator, optional gunner)
  • Length: 49 ft 7 in (15.11 m)
  • Wingspan: 66 ft 0 in (20.12 m)
  • Height: 14 ft 8 in (4.47 m)
  • Wing area: 662.36 sq ft (61.535 m2)
  • Airfoil: Zaparka
  • Empty weight: 23,450 lb (10,637 kg)
  • Gross weight: 29,700 lb (13,472 kg)
  • Max takeoff weight: 36,200 lb (16,420 kg)
  • Fuel capacity: 640 US gal (2,400 L) internal and up to four 165 US gal (625 L) drop tanks
  • Powerplant: 2 × Pratt & Whitney R-2800-65W Double Wasp 18-cylinder air-cooled radial piston engines, 2,250 hp (1,680 kW) each
  • Propellers: 4-bladed Curtiss Electric constant-speed feathering propellers, 12 ft 2 in (3.72 m) diameter.

Northrop P-61 Performance

  • Maximum speed: 366 mph (589 km/h, 318 kn) at 20,000 ft (6,100 m)
  • Range: 1,350 mi (2,170 km, 1,170 nmi)
  • Ferry range: 1,900 mi (3,100 km, 1,700 nmi) with four external fuel tanks
  • Service ceiling: 33,100 ft (10,100 m)
  • Rate of climb: 2,540 ft/min (12.9 m/s)
  • Time to altitude: 20,000 ft (6,100 m) in 12 minutes
  • Wing loading: 45 lb/sq ft (220 kg/m2)
  • Power/mass: 0.15 hp/lb (0.25 kW/kg)

Northrop P-61 Armament

  • Guns: ** 4 × 20 mm (.79 in) Hispano AN/M2 cannon in ventral fuselage, 200 rounds per gun
    • 4 × .50 in (12.7 mm) M2 Browning machine guns in remotely operated, full-traverse upper turret, 560 rpg
  • Bombs: for ground attack, four bombs of up to 1,600 lb (726 kg) each or six 5-in (127 mm) HVAR unguided rockets could be carried under the wings. Some aircraft could also carry one 1,000 lb (454 kg) bomb under the fuselage.

Northrop P-61 Image Gallery

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