Super Dragonfly
The Aircraft
Designed by pilots. Validated by engineers
Overview
Not every aircraft begins with a certification-oriented development philosophy.
The Super DragonFly was developed through systematic aerodynamic analysis, flight mechanics evaluation, structural substantiation, flight testing and independent engineering review, resulting in an aircraft where safety, stability and pilot confidence are inherently embedded into the design from the very beginning.
More than an aircraft.
An aerospace development program brought to life.
Confidence Through Engineering
The Super DragonFly was conceived around a clear objective:
delivering an aircraft that combines outstanding flying qualities, structural efficiency and operational safety through engineering—not compromise.
Inspired by the proven tandem-wing philosophy and completely redesigned from the ground up, the aircraft integrates modern composite structures, advanced aerodynamic development and a fully integrated Ballistic Recovery System into a unique aviation platform.
Every major design decision was validated through analysis, testing and technical substantiation before entering production.
Advanced Safety Features & Systems Integration
Safety by Design
Every major safety feature incorporated into the Super DragonFly follows a unified development philosophy.
Safety is not a collection of optional systems.
It is an integral part of the aircraft architecture.
Crashworthy Cockpit Safety Cell
The cockpit structure has been engineered using dedicated composite layups inspired by modern sailplane safety concepts.
It absorbs and dissipates impact energy while preserving occupant survivability during emergency landing scenarios and abnormal events.
The structure has been designed to work in conjunction with the integrated Ballistic Recovery System, providing enhanced occupant protection throughout the emergency sequence.
Fully Integrated Ballistic Recovery System
The BRS was incorporated from the earliest design stages.
Structural attachments, load paths, extraction clearances and installation requirements were engineered as part of the primary airframe structure.
Anti-Explosion Fuel Tanks
Wing-integrated fuel tanks incorporate anti-explosion technology designed to drastically reduce the risk of ignition following impact events.
This solution forms a key pillar of the aircraft's occupant protection philosophy.
Structural Roll-Over Protection
A structural roll-over protection system is integrated within the canopy framework to provide enhanced occupant protection in overturn scenarios and abnormal ground impact events.
Quick-Release Emergency Canopy System
The canopy incorporates a rapid-release mechanism enabling emergency egress under adverse conditions.
Shock-Absorbing Landing Gear
Both nose and main landing gear feature energy-absorbing systems designed to reduce loads during abnormal landing conditions and improve crash energy management.
Fire Protection Architecture
The engine compartment is separated from the cockpit by a Fiberfrax fire-resistant firewall, providing enhanced thermal protection in the event of an engine compartment fire.
Technical specifications
Aircraft ConfigurationTandem-Wing Composite Aircraft
PowerplantTitan IOX-340 ASTM Compliant
Occupants2
Maximum Power166 hp
Cockpit ProtectionCrashworthy Composite Safety Cell
PropellerMT Hydraulic Constant-Speed Propeller
Fuel SystemAnti-Explosion Fuel Tanks Integrated in Wings
Airframe ConstructionAdvanced Composite Structure
Landing GearShock-Absorbing Nose and Main Landing Gear
Ballistic Recovery SystemFully Integrated BRS
Canopy SystemQuick-Release Emergency Canopy System
Firewall ProtectionFiberfrax Fire-Resistant Firewall
Roll-Over ProtectionIntegrated Structural Roll Bar
Development PhilosophyCertification-Oriented Engineering Methodology
Designed around safety
Safety was not added to the Super DragonFly after the design phase.
It was a primary design requirement from the very beginning.
The aircraft adopts a tandem-wing configuration specifically selected to provide predictable handling qualities, benign stall behaviour and enhanced pilot confidence throughout the entire flight envelope.
Dedicated aerodynamic studies, stability assessments and flight mechanics analyses were conducted to optimize controllability, efficiency and operational safety.
The result is an aircraft designed to enable confident flying rather than requiring pilots to manage limitations.
Aerodynamics before manufacturing
The Super DragonFly was developed through a structured aerodynamic program long before manufacturing began, replacing empirical approximation with mathematical and analytical rigor.
Development activities included:
Aircraft Geometry Definition
Longitudinal Stability Assessment
Airfoil Selection and Evaluation
Directional Stability Assessment
Flight Mechanics Analysis
Canard-Wing Interaction Analysis
Neutral Point Determination
Downwash and Upwash Evaluation
Aerodynamic Performance Optimization
Every major aerodynamic characteristic was thoroughly evaluated and refined before progressing to physical validation.
Tested before production
Engineering assumptions require validation.
For this reason, the Super DragonFly development program included dedicated flight-test activities prior to construction of the final aircraft.
A scaled flying demonstrator was developed and subjected to an extensive flight campaign to validate the tandem-wing configuration and assess real-world flight behaviour.
The program accumulated hundreds of experimental flights supporting:
Stability Validation
Aerodynamic Correlation
Handling Quality Assessment
Configuration Optimization
Neutral Point Verification
The lessons learned from this experimental campaign were directly incorporated into the final aircraft design.
Structural validation
The Super DragonFly was developed using a certification-oriented structural methodology.
A complete set of flight, gust, landing and operational load cases was defined to establish the structural design envelope.
The development program included:
Structural Load Development
Vertical Tail Structural Substantiation
Finite Element Method (FEM) Analysis
Engine Mount Verification
Wing Structural Substantiation
Landing Gear Verification
Canard Structural Substantiation
Firewall Verification
Fuselage Structural Substantiation
Dedicated structural test campaigns were subsequently performed to validate analytical predictions and confirm design assumptions.
Engineering evidence supported every major structural decision.
Integrated Ballistic Recovery System
Safety extends beyond prevention.
It requires preparation for the unexpected.
The Super DragonFly was engineered from the earliest design stages around a fully integrated Ballistic Recovery System (BRS).
Unlike aircraft where recovery systems are added as optional aftermarket equipment, the parachute installation was conceived as an integral part of the core aircraft architecture.
Development activities included:
Parachute System Assessment
Ground Extraction Testing
Structural Attachment Analysis
Installation Validation
Rocket Support Verification
Continued Airworthiness Documentation
The result is a recovery solution integrated through engineering—not adaptation.
Advanced composite airframe
The aircraft is manufactured using advanced composite construction technologies designed to maximize structural efficiency, durability and repeatability.
Composite materials provide:
Optimized Structural Weight
High-Quality Aerodynamic Surfaces
Corrosion Resistance
Long-Term Durability
Enhanced Fatigue Performance
The manufacturing philosophy combines aerospace-grade engineering with practical maintainability and long-term operational durability.
Powerplant & performance
The Super DragonFly is powered by the ASTM-compliant Titan IOX-340 engine delivering 166 hp.
The powerplant is paired with a dedicated MT constant-speed propeller specifically selected to match the aerodynamic characteristics of the aircraft.
This configuration delivers an optimal balance between climb performance, cruise efficiency and operational reliability.
The aircraft was developed to provide engaging flying qualities while maintaining predictable handling and efficient operation across the entire flight envelope.
Developed as a complete aerospace development program
What differentiates the Super DragonFly within the light aviation sector is not a single feature.
It is the rigorous development philosophy behind it.
The project framework integrates:
Aerodynamics and Flight Mechanics
Comprehensive Ground Testing and Static Test Campaigns
Structural Engineering and FEM Analysis
Sub-Scale and Full-Scale Flight Validation
Means of Compliance Methodology referencing ASTM F2245, LTF-UL and CS-VLA standards
Every major design decision was supported by documented engineering evidence and validation activities, including independent review and collaboration with Leichtwerk AG, an EASA Design Organisation Approval (DOA).
This structured approach is rarely found within the light aviation sector.
Designed by pilots. Validated by engineers. Confidence Through Engineering.