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Lockheed Martin X-44 MANTA (Multi-Axis, No-Tail Aircraft)


Tailless Combat Fighter Technology Demonstrator Proposal (1999)


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The Lockheed X-44 MANTA existed as an offshoot of the then-soon-to-be F-22 Raptor line - it being a tailless aircraft relying on thrust vectoring for extreme agility.



Authored By: Staff Writer | Last Edited: 04/13/2018 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.
During the 1980s, the United States Air Force (USAF) formulated the "Advanced Tactical Fighter" (ATF) program to find America's next frontline combat fighter. This eventually led to a fly-off between the Lockheed Martin YF-22 and the Northrop Grumman YF-23 (both detailed elsewhere on this site). The former won out and the YF-22 was introduced (as the "Raptor") into service with the USAF in December of 2005 - becoming the world's first 5th Generation Fighter platform.

Even while the F-22 was in development, a heavily-modified form of the aircraft was under consideration as the X-44 "MANTA" ("Multi-Axis, No-Tail Aircraft"). This program offshoot was essentially the base F-22 Raptor design sans its tailplanes. The type was seen as a technology demonstrator to test the validity of controlling a combat fighter without traditional tailplanes being fitted. The result, showcased only through concept artwork, was an aircraft that held the front- and mid-section of the original F-22 but carried a "stretched" delta wing mainplane. It was to retain the twin, side-by-side turbofan engine arrangement with thrust-vectoring but lacked the outward-cranked vertical tail fins as well as the horizontal tailplanes.
As it stood, the aircraft would have been controlled solely by the thrust vectoring system coupled with control surfaces found on the wing mainplanes - the hope being that the fighter would have been extremely agile, offer reduced drag and greater efficiency, and keep much (if not all) of its inherent stealth properties intact. The X-44 MANTA was always seen as a possible candidate for a future combat warplane so it would also have held on to 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 would have carried more internal fuel and thus increased operational ranges when compared to the F-22.

The X-44 MANTA remained a proposed "experimental" over the course of its short life. Some interest in the product was had by both the USAF as well as NASA but little came of this for the project seems to have died off sometime around the year 2000. The X-44 designation resurfaced in another Lockheed product, this being the "X-44A", a deep-fuselage, tailless unmanned aircraft system used in the development of more advanced drones for the company (including the "Sentinel").

Specifications



Service Year
1999

Origin
United States national flag graphic
United States

Status
CANCELLED
Development Ended.
Crew
1

Production
0
UNITS


Lockheed Martin - USA
National flag of the United States United States (cancelled)
(OPERATORS list includes past, present, and future operators when applicable)
Air-to-Air Combat, Fighter
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
X-Plane (Developmental, Prototype, Technology Demonstrator)
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.


Length
62.3 ft
(19.00 m)
Width/Span
44.5 ft
(13.55 m)
Height
16.4 ft
(5.00 m)
Empty Wgt
31,967 lb
(14,500 kg)
MTOW
55,116 lb
(25,000 kg)
Wgt Diff
+23,149 lb
(+10,500 kg)
(Showcased structural values pertain to the Lockheed Martin X-44 MANTA production variant)
Installed: 2 x Pratt & Whitney F119-PW-100 afterburning turbofans developing 35,000 lb of thrust each (estimated).
Max Speed
1,553 mph
(2,500 kph | 1,350 kts)
Ceiling
49,213 ft
(15,000 m | 9 mi)
Range
1,988 mi
(3,200 km | 5,926 nm)


♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


(Showcased performance specifications pertain to the Lockheed Martin X-44 MANTA production variant. Compare this aircraft entry against any other in our database. View aircraft by powerplant type)
STANDARD:
1 x 20mm internal cannon.

AIR-TO-AIR, STEALTH:
2 x AIM-9 Sidewinders short-ranged air-to-air missiles (internal side weapons bays).
6 x AIM-120 AMRAAM medium-ranged air-to-air missiles (Internal ventral weapons bay).

AIR-TO-AIR, NON-STEALTH:
4 x AIM-9 Sidewinder short-ranged, air-to-air missiles (External, underwing, outboard)
2 x AIM-9 Sidewinder short-ranged air-to-air missiles (Internal side weapons bays).
6 x AIM-120 AMRAAM medium-ranged, air-to-air missiles (Internal ventral weapons bay).

AIR-TO-GROUND, STEALTH:
2 x AIM-9 Sidewinder short-ranged air-to-air missiles (Internal side weapons bays).
2 x AIM-120 AMRAAM medium-ranged, air-to-air missiles (Internal ventral weapons bay).
2 x 1,000lb GBU-32 Joint Direct Munitions (JDAM) (Internal ventral weapons bay).

OPTIONAL, AIR-TO-GROUND, STEALTH:
8 x 250lb GBU-39 Small Diameter Bombs (SDBs) (Internal ventral weapons bay) in place of JDAM.

OPTIONAL, MISCELLANEOUS:
2 x 600 US Gallon external fuel drop tanks underwing, inboard.


Supported Types


Graphical image of an aircraft automatic cannon
Graphical image of an air-to-air missile weapon
Graphical image of a short-range air-to-air missile
Graphical image of a medium-range air-to-air missile
Graphical image of an aircraft air-to-surface missile
Graphical image of an aircraft conventional drop bomb munition
Graphical image of an aircraft guided bomb munition
Graphical image of an aircraft external fuel tank


(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 0


X-44 MANTA - Base Project Name; cancelled.


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