/* JETX — TECHNOLOGY page content */ function ProjectsIntro() { return (
/ OverviewWhat We Do

JETX is an aerospace technology company developing the building blocks of Advanced Air Mobility — electric and hybrid-electric propulsion, a modular and scalable eVTOL platform, AI flight autonomy, and a portfolio of advanced concept aircraft for both civil and defense markets.

We design and build our own aircraft, and develop concepts on commission for government and commercial partners — bringing fighter-jet vector thrust to the AAM and UAM markets at a fraction of legacy cost.

/ The problemWhat We Are Solving

Today's eVTOL aircraft rotate or tilt their thrust sources — rotors, ducted fans, thrusters — to vector thrust for vertical flight, or rely on fixed rotors that direct thrust vertically through every stage of flight. Both add weight, noise, exposed moving parts and points of failure.

JETX's core technology removes that constraint: our thrust sources do not need to rotate or tilt to provide vertical thrust — a fundamental advantage that expands what these aircraft can do.

); } function CoreTechnology() { const specs = [ { l: "Thrust Retention", v: "98", u: "%+", n: "UCF ventral-flap CFD" }, { l: "Vectoring Response", v: "<50", u: "ms", n: "Wind-tunnel confirmed" }, { l: "Noise Attenuation", v: "15–22", u: "dB", n: "Embedded acoustic liners" }, { l: "Maintenance", v: "−60", u: "% vs rotor", n: "Fewer moving parts" }, ]; return (
COREOur Main Technology
Patent pending · validated at UCF & Tennessee Tech

Vector thrust.
Redirect it, never rotate the source.

How it works

Propulsion, fully enclosed.

A thrust source — an Electric Ducted Fan, a fluidic thruster fed by electric air compressors, or another novel electric source — is enclosed within the structure: embedded inside the fuselage, or housed in dedicated propulsion bodies and shrouded nacelles on the wings. Vector-thrust mechanisms then redirect that airflow on demand for vertical or forward flight: ventral flap, flaps, bucket and cascade vanes, all patent pending.

Because the propulsion is shrouded rather than left exposed on open rotors, the enclosure itself does acoustic work. With soundproof and thermal liners that means dramatic noise attenuation and a lower radar and thermal signature — and the modular, electric design keeps maintenance and operating cost low.

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); } function Products() { const items = [ { id: "stk-vector", num: "01 / 08", tag: "Patent Pending", title: "Vector-Thrust Propulsion", body: "Our core invention — redirect thrust with flaps, ventral flaps, bucket and cascade vanes instead of rotating or tilting the source. An Electric Ducted Fan or fluidic thruster, fully embedded, with true vertical flight and no exposed rotors.", tags: ["EDF", "Fluidic", "Ventral Flap"], img: "assets/concepts/vector-thrust-cfd.png", fit: "contain", }, { id: "stk-airflow", num: "02 / 08", tag: "Patent Pending", title: "Airflow Propulsion Systems", body: "Compresses ambient air and redirects it through embedded exhausts mixed into the vehicle geometry, for vertical or forward flight. Onboard computers drive electronic valves regulating high-pressure airflow per flight stage. Fully embeddable, electric or hybrid.", tags: ["Embedded", "Electric / Hybrid"], img: "assets/concepts/airflow-schematic.png", fit: "contain", }, { id: "stk-power", num: "03 / 08", tag: "Army Validated", title: "Hybrid-Electric Power", body: "Vendor-agnostic power from 90 kW to 1 MW+ across three modes — silent electric, hybrid cruise and full turbogenerator. Multi-fuel by design: Jet-A1, Diesel, AVGAS, SAF and Hydrogen, with endurance from 179 to 642 minutes.", tags: ["Multi-Fuel", "90 kW → 1 MW+"], slides: ["assets/concepts/hybrid-cutaway.png", "assets/concepts/hybrid-pods-system.png"], }, { id: "stk-ai", num: "04 / 08", tag: "Air Force Validated", title: "AI Autonomy", body: "Onboard AI fuses multi-source data and runs real-time Monte-Carlo simulations to fly the optimal path — 80% mission success across 500+ engagements on combat simulators at 25X speed under U.S. Air Force contracts.", tags: ["GPS-Denied", "Sim-to-Real"], slides: ["assets/concepts/apex-sim.png", "assets/concepts/apex-coa-dashboard.png", "assets/concepts/apex-coa-flow.png"], }, { id: "stk-airframes", num: "05 / 08", tag: "Mission-Optimized", title: "Novel Airframes", body: "Purpose-built vector-thrust platforms — high-wing twin-tail for naval and ISR, canard configurations for speed, and flying-wing designs with low-observable features for military strike.", tags: ["Twin-Tail", "Canard", "Flying-Wing"], img: "assets/concepts/novel-airframes-v2.png", }, { id: "stk-modular", num: "06 / 08", tag: "All eVTOL Classes", title: "Modular & Scalable Platform", body: "One platform performing the duties of helicopters and tilt-rotors at a fraction of the cost. The body is a module — swap it for cargo, passenger, medical, ISR, delivery or firefighting.", tags: ["Swappable Body", "Rapid Variants"], slides: ["assets/concepts/modular-clear-1.png", "assets/concepts/modular-clear-2.png"], }, { id: "stk-civil", num: "07 / 08", tag: "Civil", title: "Civil eVTOL Aircraft", body: "A portfolio of passenger, cargo and amphibious eVTOLs — from two-seat personal craft to six-seat cabins — built on JETX propulsion and platform technology for on-demand air taxi, logistics and personal mobility.", tags: ["Passenger", "Cargo", "Amphibious"], img: "assets/concepts/n03.png", }, { id: "stk-defense", num: "08 / 08", tag: "Defense", title: "Defense & Military Aircraft", body: "Mission-optimized unmanned and manned platforms — tactical UAVs, stealth flying-wings and munitions carriers — bringing fighter-jet vector thrust to ISR, reconnaissance, strike and resupply.", tags: ["Unmanned", "Stealth", "ISR / Strike"], img: "assets/concepts/defense-aircraft.png", }, ]; return (
DEVOur Development
One technology stack · civil & military

Beyond vector thrust.
The complete stack.

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); } function FlagshipX2S() { const specs = [ { v: "300 kg", l: "Modular Payload" }, { v: "22 min", l: "Silent Low-Signature" }, { v: "TRL 6", l: "Maturity" }, { v: "GPS-Deg.", l: "Autonomous Nav" }, ]; return (
X2SFlagship Platform
Submission 4-26-0226 · Awardable · May 28 2026

The X2S.
Award-ready for the U.S. Army.

X2S · GROUP IV · NON-ROTATING VECTOR THRUST
Award-Ready · DevX Autonomy

Multi-Mission Defense UAV

A next-generation tactical UAV built around proprietary non-rotating vector thrust — redirecting thrust without rotating motors or moving nacelles for fewer failure points and greater control authority. It pairs helicopter vertical access with fixed-wing speed, powered by a hybrid-electric propulsion system with a multi-fuel turbogenerator, supporting ISR, reconnaissance and resupply with autonomous maneuvering in GPS-degraded environments. Designated Awardable on the U.S. Army DevX Autonomy marketplace.

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); } function ProtoTesting() { const items = [ { id: "poc-1", size: "g-half", fit: "contain", src: "assets/concepts/poc-flap-pole.png" }, { id: "poc-2", size: "g-half", fit: "contain", src: "assets/concepts/poc-twin-edf.png" }, { id: "poc-3", size: "g-third", fit: "contain", src: "assets/concepts/poc-nozzle-gantry.png" }, { id: "poc-4", size: "g-third", fit: "contain", src: "assets/concepts/poc-smoke.png" }, { id: "poc-5", size: "g-third", fit: "contain", src: "assets/concepts/poc-nozzle-pair.png" }, { id: "poc-6", size: "g-half", fit: "contain", src: "assets/concepts/poc-flap-pair.png" }, { id: "poc-7", size: "g-half", fit: "contain", src: "assets/concepts/poc-tri-assembly.png" }, ]; const ttu = [ { id: "pt-windtunnel", size: "g-half", fit: "cover", src: "assets/concepts/ttu-windtunnel.png" }, { id: "pt-edf-module", size: "g-half", fit: "cover", src: "assets/concepts/ttu-rig.png" }, { id: "pt-cfd", size: "g-third", fit: "cover", src: "assets/concepts/ttu-edf.png" }, { id: "pt-bench", size: "g-third", fit: "cover", src: "assets/concepts/ttu-nozzle.png" }, { id: "pt-subscale", size: "g-third", fit: "cover", src: "assets/concepts/ttu-loadrig.png" }, ]; return (
LABPrototypes & Proof of Concept
Proof-of-concept prototypes · tested 2021

Built and tested.
Not just rendered.

Every JETX claim is grounded in analysis and hardware. UCF computational fluid dynamics maps velocity and thrust across EDF, ventral-flap and cascade configurations; at the Tennessee Tech subsonic wind tunnel we then measured thrust, vectoring authority and stability — validating multi-axis control on three-fan rigs and capturing force and moment data on a six-DOF stand. Together these campaigns de-risk the propulsion architecture long before it reaches flight.

Proof of Concept · 2021
{items.map((it) => (
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Tennessee Tech · Wind-Tunnel & Bench Testing
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UCF · Computational Fluid Dynamics
); } function ProjectsPage() { return ( ); } window.mountPage("projects.html", ProjectsPage);