
Lockheed Martin X-44 MANTA
Aircraft
The
X-44 MANTA (Multi-Axis No-Tail Aircraft) was a
conceptual Lockheed Martin aircraft
design that has been studied by NASA
and the
U.S. Air Force. It was intended to test the
feasibility of full yaw, pitch and roll control without
tailplanes (horizontal or vertical). Attitude
manipulation relies purely on 3D
thrust
vectoring.
The aircraft itself was an
F-22
Raptor-derived design featuring a stretched version of the
delta wing and deleted tail surfaces.
Funding for the X-44 program was ended in 2000.
"X-Planes Explained". NASAExplores.com, October
9, 2003
Design and development
The X-44 was designed by Lockheed Martin to demonstrate the
feasibility of an aircraft controlled by vectored thrust alone. The
X-44 design had a reduced radar signature and was made more
efficient by eliminating the tail and rudder surfaces, and instead
using thrust vectors to provide yaw, pitch and roll control.
The X-44 MANTA design was based on the F-22, except without a tail
and incorporated a full delta wing. The basic X-44 MANTA will
entail a larger weapons payload and a greater fuel capacity than
the F-22. The X-44’s delta wing would allow it to carry more
weapons and fuel. The MANTA was designed to have reduced mechanical
complexity, increased fuel efficiency and greater agility. The X-44
MANTA combined the control and propulsion systems, using
thrust vectoring.
The X-44 MANTA was an experimental design that was never brought to
reality.
See also
References
- Pike, John. "X-44 MANTA." GlobalSecurity.org, 27 April
2005.
External links