
SYSTEM CONTROL
Aero-native system control adaptable for hybrid systems
THERMAL MANAGEMENT
Integrated systems to optimise system thermal efficiency, profiled to minimise drag reduction
BLENDED WING
Lift to drag ratio: 20
FUEL CELL STACK
Capitalizing on technology advances through competitive supply chain
ELECTRICAL SYSTEMS
Significant mass optimizatino - highly competitive
STRUCTURAL HYDROGEN STORAGE
Optising aircraft structure via structurally integrated storage, to maximise gravimetric energy density
ST-5 STINGRAY: Hydrogen-Native UAV
AIRCRAFT DESIGN & INTEGRATION
Building upon CAeS heritage in drone design and integration and following on from key concept aircrafts such as X-48B/C design to maximise flight efficiency
SCALABLE/ ADAPTABLE PLATFORM ARCHITECTURE
Supporting both civil and defence application, scaled for different mission profiles
DISTRIBUTED POWERTRAIN SYSTEMS
Optimised architecture to support aircraft mass and balance. This includes distributed H2 storage
FLIGHT ENDURANCE
Designed to maximise operational performance , benefitting from maximising system gravimetric density
MAXIMISING CARGO
Designed to support standard crate size and structured to maximise turnaround times

ST-5 STINGRAY (8 KW)
WINGSPAN: 5.5M
LENGTH: 7M
CROSS WIND TOLERANCE: 10M/S
CRUISE SPEED: MORE THAN 33M/S
PAYLOAD: 5-55 KG
ENDURANCE: 19 HRS
ST-7 STINGRAY (35 KW)
WINGSPAN: 7.4M
LENGTH: 8M
CROSS WIND TOLERANCE: 10M/S
CRUISE SPEED: MORE THAN 33M/S
PAYLOAD: 80-120 KG
ENDURANCE: 40 HRS
ST-15 STINGRAY (100 KW)
WINGSPAN: 15M
LENGTH: 10M
MAX CLIMB RATE: 900FPM
PAYLOAD: 350 KG
ENDURANCE: 40 HRS
ST-18 STINGRAY (800 KW)
WINGSPAN: 18M
LENGTH: 12M
MAX CLIMB RATE: 900FPM
PAYLOAD: 2,000 KG
ENDURANCE: 10 HRS

DESIGN
JUNE 2025

MANUFACTURE
OCT/NOV 2025

SYSTEMS FLIGHT TEST
OCT/NOV 2025












