History of the Lockheed Martin X-44 MANTA (multi-rotor tailless aircraft)

In the 1980s, the United States Air Force (USAF) developed the Advanced Tactical Fighter (ATF) program to find America's next front-line fighter. This eventually led to the flight between the Lockheed Martin YF-22 and the Northrop Grumman YF-23 (both are detailed elsewhere on this page).

The former won, and the YF-22 (as the "Raptor") entered service with the US Air Force in December 2005 - becoming the world's first 5th generation fighter platform.

Even during the development of the F-22, a significantly improved form of the aircraft was considered, namely the X-44 "MANTA" ("multi-rotor tailless aircraft"). This branch is essentially the basic design of the F-22 Raptor minus its tail.

The type is seen as a technology demonstrator to test the effectiveness of controlling a fighter jet without installing a conventional tail. Presented only through concept art, the result is an aircraft that combines the front and center of the original F-22, but with a "stretched" delta-wing main aircraft.

It was intended to retain the configuration of two side-by-side turbofans with thrust vectoring, but lacked the outwardly curved vertical and horizontal fins.

For now, the aircraft will be controlled solely by a thrust vectoring system combined with control surfaces on the wing main aircraft - hopefully the fighter will be extremely maneuverable, provide less drag and greater efficiency, and can accommodate Many, if not all, of its inherent stealth characteristics remain intact. The X-44 MANTA has long been seen as a possible candidate for a future fighter, so it would also be in line with the F-22's internal weapons bay.

Due to the nature of the delta wing and its large surface area and increased internal volume, the MANTA will carry more internal fuel than the F-22 and therefore have a greater range.

The X-44 MANTA remained a proposed "experiment" in its short life. Both the U.S. Air Force and NASA were interested in the product, but with little success, as the program appeared to be terminated sometime around 2000.

The X-44 name reappears in another Lockheed product, the "X-44A," a deep-body tailless unmanned aerial system used to develop more advanced UAVs for the company (including "sentinel").

Lockheed Martin X-44 MANTA (multi-rotor tailless aircraft)

Basic

Year:
1999
Status:
Cancel
Staff:
1

Production

[0 units]:
Lockheed Martin - USA

Roles

- Fighter

- X-Plane / Development

Dimensions

Length:

62.34 ft (19 m)

Width:

13.55m

Height:

16. 40 feet (5 m)

Weight

Curb Weight:

14,500 kg

MTOW:

25,000 kg

(difference: +23.149lb)

Performance

2 x Pratt & Whitney F119-PW-100 afterburner turbofans, 35,000 lb thrust each.

Performance

Maximum Speed:

1,553 mph (2,500 km/h; 1,350 knots)

Service Limit:

49,213 ft (15,000 m; 9.32 mi)

Maximum range:

1,988 miles (3,200 km; 1,728 nautical miles)

Armor

Default:

1 x 20mm inner gun.

Air-to-air, invisible:

2 x AIM-9 Sidewinders short-range air-to-air missiles (internal side weapons bay).

6 x AIM-120 AMRAAM medium-range air-to-air missiles (internal ventral weapons bay).

Air-to-air, non-stealth:

4 x AIM-9 Sidewinder short-range air-to-air missiles (external, underwing, outboard)

2 x AIM-9 Sidewinder short-range air-to-air missiles (internal side weapon bay).

6 x AIM-120 AMRAAM medium-range air-to-air missiles (internal ventral weapons bay).

Air-to-Ground, Stealth:

2 x AIM-9 Sidewinder short-range air-to-air missiles (internal side weapon bay).

2 x AIM-120 AMRAAM medium-range air-to-air missiles (internal ventral weapons bay).

2 x 1,000lb GBU-32 Joint Direct Ammunition (JDAM) (internal ventral weapons bay).

Optional, air-to-ground, stealth:

8 x 250 lb GBU-39 Small Diameter Bomb (SDB) (internal ventral weapons bay) instead of JDAM.

optional, miscellaneous:

2 x 600 US gallon external underwing fuel tanks, inboard.

Changes

X-44 MANTA - Base item name; cancelled.

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