Lockheed XP-58 Chain Lightning

https://en.wikipedia.org/wiki/Lockhe...hain_Lightning

Design and development​

The Lockheed XP-58 Chain Lightning was an American long-range fighter developed
during World War II. Although derivedfrom the successful P-38 Lightning, the
XP-58 was plagued by technical problems with its engines that eventually led to
the project's cancellation.

The XP-58 was a Lockheed Aircraft Company funded initiative to develop an
improved Lightning as a long-range fighterfollowing the release by the U.S. Army
Air Corps of the Lightning for sale to Britain on 20 April 1940. Initially, two
designs were formulated, both using the Continental IV-1430 engines. One would
be a single-seat aircraft with one 20 mm (.79 in) cannon and four .50 in (12.7
mm) machine guns. The second would be a two-seat aircraft with the addition of a
flexible .50 in (12.7 mm) gun at the end of each tail boom.

In July 1940, Lockheed decided to switch to Pratt & Whitney XH-2600 engines as
the aircraft would be underpowered with the Continental engines, with the
aircraft having two seats and designated "XP-58". However, soon Lockheed was
advised the development of the XH-2600 engine was terminated. After
consideration of the engine alternatives, the design was changed to use two
Wright R-2160 Tornado engines, as well as a change of the rear-facing armament
to two turrets, one upper and the other lower on the fuselage, each turret
containing two .50 in (12.7 mm) machine guns. As support equipment for the two
crewmen was added, the estimated weight of the XP-58 grew to 34,232 lb (15,527
kg) by August 1941.

In March 1942, the USAAF placed an order for a second XP-58 that would
incorporate increased fuel tanks to obtain a range of 3,000 mi (4,800 km). The
Air Force were uncertain about the role and armament of the aircraft, and in
September 1942, a decision was made to convert the aircraft for a role as a
low-altitude attack aircraft, armed with a 75 mm (2.95 in) M5 autocannon.
Adequate aircraft were already available for this mission, with the Douglas A-26
Invader and Beechcraft XA-38 Grizzly under development. As a result, the second
XP-58 was canceled and the role of the design reverted to that of a
high-altitude fighter, using large-bore cannon firing high-explosive shells to
break up bomber formations.

The 37 mm (1.46 in) M4 autocannon was originally selected for a quadruple mount
in the nose, but the trajectory of the 37mm shells dropped lower than other
weaponry, limiting its effective range. A hydraulically articulated nose that
could be bent up to correct this problem was tried, but was dismissed as too
complex. Then, a 75 mm (2.95 in) M5 autocannon paired with twin .50 in (12.7 mm)
machine guns was tried and proved much more successful.

Role
Heavy fighter

Manufacturer
Lockheed

First flight
6 June 1944

Status
Canceled

Number built
1

Developed from
Lockheed P-38 Lightning

Testing​

In February 1943, use of another engine, the Allison V-3420, was necessary due
to poor progress with the Tornado engine development. With this change, the
second XP-58 was resurrected. The XP-58 had its first flight on 6 June 1944, but
flight test work on the XP-58 took second place to other higher priority
developments. Eventually, 25 test flights were completed. The XP-58 was then
flown to Wright Field for USAAF acceptance tests, even though the
turbo-superchargers were experiencing torching and a number of systems were not
installed including provision for cockpit pressurization and armament with its
fire-control equipment. Although the prototype arrived at Wright Field on 22
October 1944, the aircraft was a maintenance headache and no further trials were
conducted. The construction of the second prototype was abandoned.


Specifications (XP-58)​

General characteristics
Crew: two, pilot and gunner
Length: 49 ft 5.5 in (15.07 m)
Wingspan: 70 ft 0 in (21.34 m)
Height: 16 ft 0 in (4.88 m)
Wing area: 600 sq ft (55.7 m2)
Empty weight: 31,624 lb (14,344 kg)
Max takeoff weight: 39,192 lb (17,777 kg)
Powerplant: 2 × Allison V-3420 24 cylinder liquid-cooled engine, 3,000 hp (2,238
kW) each

Performance
Maximum speed: 436 mph (702 km/h, 379 kn) at 25,000 ft (7,620 m)
Cruise speed: 283 mph (455 km/h, 246 kn)
Range: 2,650 mi (4,265 km, 2,304 nmi)
Service ceiling: 38,200 ft (11,645 m)
Rate of climb: 2,582 ft/min (13.1 m/s)

Armament

Guns:
(proposed) 4 × 37 mm (1.46 in) M4 cannons or 1 × 75 mm (2.95 in) M5 cannon and 2
× .50 in (12.7 mm) Browning heavy machine guns in interchangeable nose proposed)
4 × .50 cal (12.7 mm) Browning heavy machine guns in two remotely controlled
flexible turrets in the rear.




*