Prototype X-BAT VTOL ‘Fighter’ Drone Unveiled
Shield AI has shared the first look at a full-scale prototype of its X-BAT jet-powered stealth ‘fighter’ drone, which is designed to both take off and land vertically from a tail-sitting position. This is the company’s latest step toward proving out what remains an extremely ambitious aircraft concept. The tailless X-BAT has already received a significant vote of confidence from the U.S. Navy, which is hoping to see the drone develop into a real operational capability on a very aggressive timeline.
A video showing X-BAT 001, the first of two full-scale prototypes Shield AI plans to build, was released earlier today and is seen below. The drone is in the process of being moved from the company’s main hub in Frisco, Texas, to its flight test facility in Newton, Kansas. These sites are also known as X-Forge 1 and X-Forge 2, respectively. X-BAT was revealed to the public last year, as TWZ was first to report on in depth.
X-BAT has already evolved significantly since its unveiling. In April, a half-scale model was displayed at the Navy League’s Sea-Air-Space 2026 exposition, showing major changes to the core design. The entire planform was reworked from a ‘cranked kite’ type arrangement to one with an arrowhead-shaped profile featuring a straight leading edge with a more dramatic sweep.
The configuration of the X-BAT 001 prototype is broadly reflective of the model seen at Sea-Air-Space this year, as well as more recent computer renderings. However, there are some notable differences.
For one, the prototype’s thrust-vectoring exhaust nozzle extends significantly to the rear of the drone beyond the trailing edges of the wings. Previously shown models and renders had the nozzle in a position more inset in the rear fuselage.
A side-by-side comparison of X-BAT 001’s exhaust nozzle configuration, at left, and the arrangement of the nozzle seen on the half-scale model at Sea-Air-Space 2026 in April. Shield AI capture/Jamie Hunter
There are also two pronounced bulges toward the rear of the central body, one on either side of X-BAT 001’s dorsal ‘spine.’ These do not appear to be present on any models or renderings shown in the past. Each one of the bulges also has a small opening at the front. There are two circular openings on top of the spine with mesh screens covering them, as well. Small fans may be visible inside them.
The purpose of these features on top is unknown, and Shield AI declined to comment when asked for more information. They could be tied to the drone’s propulsion arrangement. The drone’s thrust-vectoring exhaust nozzle only provides pitch and yaw control. Shield AI has said in the past that bleed air routed through thrusters in the wings will be used for roll control.
A top-down look at X-BAT 001, showing the bulges on either side of the dorsal ‘spine,’ as well as the circular openings. Shield AI capture
Various panel lines with circular edges are also visible across the top of the drone. This is distinctly different from the saw-tooth-edged paneling depicted on previously shown models and renders.
Another full look at X-BAT 001 from the front quarter. Shield AI capture
As an aside, the prototype also features an insignia on the top of its left wing with a skull and other motifs, which the company says is meant to pay homage to all four branches of the U.S. military.
A close-up look at the ‘skull’ insignia. Shield AI capture
“X-BAT 001 is a development aircraft, so the design will evolve as we test and refine it,” a Shield AI spokesperson also told TWZ today.
Shield AI had previously said that the prototype nozzle arrangement would lack low-observable (LO) attributes, but also that this would change after initial testing. From what we can see now, the experimental nozzle is well blended considering the current stage of development. Beyond that, it has what appears to be remarkably good low-observable (stealthy) optimization, especially true for a prototype. Initial examples of new designs are often cluttered with elements that are eliminated later on, like antennas and air data probes. Some of these features could be added to X-BAT 001 prior to flight testing.
In an interview with TWZ last month, Shield AI’s Armor Harris, Senior Vice President and General Manager of the company’s aircraft division, had also compared the expected differences between the full-scale prototypes and production version “as like X-35 versus F-35.” This is a reference to Lockheed Martin’s X-35 demonstrators, which were broadly similar, but also distinctly different from the production variants of the Joint Strike Fighter.
“That’s a full-scale vehicle,” Harris also stressed when talking about the configuration of the full-scale prototypes. “It’s got the outer mold line, it’s got the F110 engine, the full propulsion path, everything in it.”
The “propulsion path” mentioned here, which includes the aforementioned exhaust nozzle and thrusters, is absolutely critical to the X-BAT concept. The design leverages past work on an Axisymmetric Vectoring Exhaust Nozzle (AVEN), first developed in the 1990s for an experimental thrust-vectoring F-16 fighter. Shield AI has been using the original test nozzle, which had been in storage for decades, as part of the development process.
No runway, no problem.
Shield AI and @GE_Aerospace just cleared a critical path to vertical flight, completing engine light-off testing of the Axisymmetric Vectoring Exhaust Nozzle (AVEN) for X-BAT.
Engineers from both companies integrated the AVEN into GE Aerospace's… pic.twitter.com/OxV3y3sRKB
— Shield (@shieldaitech) July 20, 2026
X-BAT’s ability to take off and land vertically comes down to this propulsion arrangement combined with guidance, navigation, and control (GNC) systems. The GNC elements will leverage Shield AI’s experience with the much smaller, internal combustion-engine-powered, tail-sitting V-BAT. This, in turn, creates benefits from the design perspective, especially obviating the need for any kind of landing gear, and opens the door to a host of new operational possibilities. X-BAT is desi
Source: www.twz.com — article syndicated from the publisher’s feed; all rights remain with the original publisher.