SYSTEMS ONLINE REV. 04 / 26
LAT 52°13'NLON 21°01'E ALT 00.000 m HDG 087°
FLIGHT READY V-DYN / VLS-04
Velaris unmanned aerial platform on high-speed approach over mountain terrain
VLS-DYN / ADV. AERIAL PROPULSION

High-Speed Aerial Systems & Turbojet Propulsion.

Engineered for Speed. Built for Scale.

Velaris Dynamics develops integrated unmanned aerial systems and proprietary turbojet propulsion technologies designed for high-speed, long-range, and scalable deployment — combining propulsion engineering, airframe design, and system integration into operationally relevant aerial capabilities.

Four disciplines.
One integrated
aerial capability.

Our approach fuses propulsion engineering, airframe design, and system integration — so each platform is developed as a whole, not as the sum of off-the-shelf parts. From bench-level turbojet cores to flight-ready air vehicles, Velaris controls the full stack.

/ 01

Compact
Turbojet
Engines

Proprietary cores engineered specifically for unmanned aerial applications.

/ 02

High-Speed
Aerial
Platforms

Modular, long-range UAVs engineered for high-speed flight regimes.

/ 03

Integrated
Propulsion +
Airframe

Delivered as complete systems — matched, tuned, and flight-qualified.

/ 04

Scalable
Production
Engineering

Architected from day one for repeatable, cost-focused manufacturing.

Velaris delivers both standalone turbojet propulsion systems and fully integrated aerial platforms — bridging the gap between low-performance propulsion and high-cost traditional aerospace.

SECTOR 01 / SYSTEMSSYSTEMS

Modular
air vehicles.
Mission-adaptive by design.

Velaris develops advanced unmanned aerial platforms engineered for high-speed flight and extended operational range. Each airframe is treated as a configurable system — built to absorb evolving mission profiles, payload architectures, and deployment doctrines without redesign.

Velaris Dynamics MTJD next-generation aerial platform over cloud layer at dusk
MTJD-04 · High-Speed UAV · Cruise Profile VLS/REC-0142 · 26.04
DECY_SPRITE · PLATFORM BRIEF CLS-A · REV 02
Range< 1,000 km
Max Cruise Speed1,060 km/h
Cruising Altitude15,000 ft
OEW42 kg
Payload15 kg
MTOW85 kg
Length2.9 m
Wing Span2.4 m
LAUNCH: CONVENTIONAL · MOBILE · SRB MODE: OBSERVATION / STRIKE
Platform Characteristics
  • /01High-speed flight capability across subsonic and transonic regimes
  • /02Extended range performance optimised for endurance-critical missions
  • /03Modular payload architecture, swappable in field conditions
  • /04Configurable mission profiles — ISR, strike, test & evaluation
  • /05Production-oriented design with reduced part count
System-Level Design

Each platform is developed as an integrated system — propulsion matched to mission profile, aerodynamic geometry optimised for high-speed regimes, and structural design aligned with manufacturing constraints from the earliest development phases.

Regime
Subsonic → Transonic
Launch
Runway · Rail · SRB
Recovery
Conventional · Parachute
Autonomy
Waypoint · GNSS-Denied
SECTOR 02 / PROPULSIONPROPULSION

Compact cores.
Aerospace-grade
thrust.

Velaris develops compact turbojet engines specifically engineered for unmanned aerial applications — addressing the critical gap between underpowered commercial micro-turbines and prohibitively expensive traditional aerospace engines.

VLS-CORE / TURBOJET UNIT
MTJD-04
Micro Turbojet · Propulsion Demonstrator
1.42T/W
Thrust-to-Weight
85KRPM
Max Shaft Speed
900°C
TET Operating
Key Capabilities
  • /01High thrust-to-weight performance across operating envelope
  • /02Compact architecture designed to integrate with modern airframes
  • /03Stable operation across full mission profiles
  • /04Engineered for drop-in integration with Velaris platforms
Engineering Approach
/01CFD ModelingAdvanced flow analysis across the full compressor-turbine stageANALYSIS
/02FEM · ThermalStructural & thermal analysis validated against hot-section testSTRUCTURAL
/03Combustion TuningAnnular combustion system optimised for fuel flexibilityCOMBUSTION
/04High-Speed RotatingRotor dynamics, bearing architecture and balancingDYNAMICS
Materials & Construction
Hot Section
Ni-Based High-Temperature Alloys
Structure
Titanium Precision Components
Machining
5-Axis Precision / Grinding
Additive
LPBF · Integrated Cores

Propulsion is treated as a core system driver — enabling high-speed flight, extending operational range, and reducing mission cost.

SECTOR 03 / ENGINEERINGMANUFACTURING

A direct line
from design
to production.

Velaris develops technologies with a clear, deliberate path to manufacturing. Every geometry, fastener, and fluid path is justified against production logic — so what is proven at TRL 5 does not have to be re-engineered at TRL 8.

PHASE 01 DSG
System
Architecture
Integrated propulsion, airframe and avionics defined as one coupled system from requirements capture.
↳ 02
PHASE 02 SIM
Aerodynamic &
Thermal Modeling
High-fidelity CFD + thermal coupling across the full envelope, correlated against flight-representative test.
↳ 03
PHASE 03 STR
Structural
Optimisation
FEM-driven structural refinement balanced against mass budget, stiffness and manufacturing constraints.
↳ 04
PHASE 04 INT
Integration
Engineering
Sub-system integration validated on-bench and in flight — propulsion to airframe, power, sensors, payload.
↳ MFG
Manufacturing Strategy
  • /01Simplified component architecture — fewer interfaces, fewer failure modes
  • /02Reduced part count across propulsion and airframe families
  • /03Scalable production processes targeting serial output
  • /04Cost-focused design decisions, made early and irreversibly
Industry Context
  • /01Modern aerospace demands rapid development cycles
  • /02Repeatable, qualified production — not artisanal one-offs
  • /03Scalable output aligned with operational tempo
  • /04Velaris is designed from day one to meet these requirements
×3FASTER TO SERIES

Velaris technologies are designed to meet production requirements from the outset — not bolted on once the prototype flies.

SECTOR 04 / APPLICATIONSAPPLICATIONS

Engineered for
operators
at the edge.

Velaris technologies support a wide range of aerial applications — from long-range unmanned systems to advanced aerospace test programs. The same propulsion cores and airframe families adapt across mission domains without re-engineering.

/01
Long-Range
Unmanned Systems
Extended-endurance platforms operating beyond tactical range.
/02
High-Speed
Aerial Platforms
Transonic-capable vehicles for time-critical missions.
/03
Test &
Evaluation Vehicles
Reconfigurable airframes for propulsion and sensor trials.
/04
Infrastructure
Monitoring
Wide-area inspection of critical linear infrastructure.
/05
Security &
Surveillance
Persistent, high-altitude observation of denied areas.
/06
Advanced
Aerospace Programs
Collaborative development for national and allied industries.

Market direction
driving demand.

The shift toward autonomous systems, distributed operations, and scalable aerial capabilities is redefining what propulsion and platform technology must deliver — at speed, at range, and at production tempo.

  • Autonomous Systems
  • Distributed Operations
  • Scalable Aerial Capability
  • Sovereign Propulsion
Unmanned aerial platform cruising over canyon terrain

A vertically
integrated
aerial stack.

Velaris owns the propulsion science, the airframe physics, and the production logic that turns them into flight-qualified hardware. That combination is rare — and it is the difference between a demonstrator and a fielded system.

Request Capabilities Brief
01
Proprietary Propulsion
Compact turbojets engineered in-house — not rebadged commercial cores.
02
Matched Airframes
Platforms designed around the engine, not the other way around.
03
Production DNA
Serial manufacturability is a design requirement, not a retrofit.
04
Sovereign Capability
End-to-end IP ownership — from combustor to control surface.

Engineered
for speed.
Ready to talk.

For platform enquiries, propulsion licensing, joint programs or partnership briefings — reach the Velaris Dynamics team directly. We respond within one operational day.

HQ San Antonio

Open Briefing Channel

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