ORBITER

ENGINEERED FOR ALTITUDE. DESIGNED FOR ENDURANCE

SYSTEM OVERVIEW

High-Altitude Long-Endurance Aerial System
Engineered for Altitude. Designed for Endurance.

Orbiter high-altitude platform

ORBITER is a High-Altitude Long-Endurance (HALE) UAV developed for missions where altitude, persistence and efficiency define operational success.

Derived from certified sailplane architecture and enhanced through advanced unmanned systems integration, ORBITER combines aerodynamic efficiency, structural maturity and mission flexibility within a single high-altitude platform.

Rather than scaling a conventional UAV architecture, ORBITER has been engineered from the ground up as an endurance-driven aerospace system optimized for sustained operations, efficiency and reliability.

AERONAUTICAL HERITAGE, UNMANNED EVOLUTION

ORBITER originates from a certified sailplane-based configuration selected for its exceptional aerodynamic efficiency and long-duration flight capability.

Its design philosophy combines proven aeronautical principles with advanced unmanned mission architecture, creating a platform optimized for very high operating altitudes, reduced energy consumption and extended mission endurance.

The result is a HALE platform capable of delivering persistent aerial presence where altitude, efficiency and endurance become operational advantages.

MISSION-DRIVEN BY DESIGN

Orbiter mission profiles

ORBITER is designed to provide persistent presence and wide-area coverage from high altitude, supporting long-duration observation, sensing and communication missions.

Persistent Surveillance & Observation

Continuous monitoring over large areas with extended mission endurance and broad operational coverage.

Environmental Monitoring & Advanced Sensing

EO/IR, LiDAR and multispectral payloads supporting mapping, environmental monitoring and reconnaissance applications.

Communication Relay Operations

Extended communication coverage and data relay capabilities across remote and challenging operational environments.

Atmospheric & Scientific Research

Data collection missions within the upper troposphere and lower stratosphere for scientific and environmental applications.

Meteorological Monitoring

Weather observation and atmospheric analysis missions requiring persistence, stability and operational altitude.

Strategic Support Missions

Long-endurance aerial support for wide-area monitoring and information gathering activities.

TECHNICAL SPECIFICATIONS

Orbiter technical specifications
Wingspan 19-22 meters MTOW 1.000 kg

Wingspan19-22 m

MTOWUp to 1,000 kg

Payload CapacityUp to 400 kg

Operational CeilingUp to 21,000 m / 65,000 ft

EnduranceUp to 32 Hours

Operating SpeedLow-Speed Loitering to High-Speed Cruise

PropulsionMOGAS / Diesel / Hybrid

OperationsAutonomous Flight with Human-in-the-Loop Supervision

PayloadsEO/IR, LiDAR, Multispectral and Mission-Specific Sensors

AERODYNAMICS AS THE FOUNDATION

For HALE aircraft, aerodynamic efficiency is not a feature. It is the foundation of the entire system.
ORBITER has been developed around a high-efficiency aerodynamic architecture combining:

High-aspect-ratio wing design

Dedicated high-altitude airfoils

Low-drag fuselage configuration

Optimized wing-fuselage integration

High lift-to-drag ratio

The aerodynamic configuration has been refined through advanced Computational Fluid Dynamics (CFD) analyses, including pressure distribution assessment, drag reduction studies and laminar flow behaviour prediction.

SYSTEM ARCHITECTURE DESIGNED FOR EVOLUTION

ORBITER is conceived as a system-level platform where airframe, propulsion and mission payloads are integrated from the earliest design stages.

Its scalable multi-propulsion architecture has been developed to support evolving mission requirements while preserving efficiency, reliability and operational flexibility.

Key Architectural Features

Multi-Propulsion System Concept

Optimized Thrust Distribution

Pusher Propulsion Layout

Sensor-Friendly Undisturbed Airflow

MOGAS, Diesel or Hybrid Propulsion Options

Mission-Oriented Scalability

Autonomous Operations with Human-in-the-Loop Supervision

The pusher configuration allows mission sensors to operate in cleaner airflow conditions, maximizing sensor performance and mission effectiveness.

DESIGNED WITH AIRWORTHINESS IN MIND

ORBITER has been developed following a certification-oriented engineering philosophy.
The platform leverages certified sailplane design principles adapted to unmanned and high-altitude operations, combining proven aeronautical methodologies with modern UAV system integration.

The engineering process incorporates:

Structural Sizing and Load Analysis based on recognized airworthiness methodologies

FEM-Based Structural Validation

Aeroelastic Assessment

System Safety Considerations

Compliance-Aware Design Choices

Traceable Development Methodology

ORBITER is not conceived as a technology demonstrator. It is engineered as an operational platform developed for reliability, traceability and long-term deployment.

ORBITER

Persistent Altitude. Efficient Endurance.

ORBITER combines certified aeronautical heritage, advanced unmanned systems integration and certification-oriented engineering into a new generation of High-Altitude Long-Endurance platforms.

Where endurance becomes capability.

Orbiter in flight

ORBITER