Vian

Future Ready Hybrid Propulsion Autonomous Shuttle

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Decoupled hybrid propulsion to maximize mission success
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Autonomous Mission Control with remote piloting capability
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Whisper quiet and flexible physical profile to maximize usability in challenging environments
Payload
2,200 LBs
Crew
Autonomous
Emissions
↓ 70%+
Noise Profile
< 50 dB

Development Milestones

Flight One
Collecting data and validating flight characteristics
3.5 Ft Model
Build
Flight One
Collecting data and validating flight characteristics — 3.5 Ft Model
Digital Design
Digital drawings and digital testing
5' Model
Build with more realistic materials & jet engines

Capability Matrix

Engineering subsystems composing the Vimana platform. All specifications represent target operational envelope.

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Propulsion Architecture

DUAL-HYBRID / LIFT MATRIX

Decoupled hybrid propulsion lift system which utilizes biofuel to allow shuttle to enjoy instant VTOL "jump" capability as well rapid descent along with battery trickle charging while en route.

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Aerodynamic Design

VARIABLE-GEOMETRY HIGH-LIFT

Variable-Geometry High-Lift Segmented Wings. High-mounted, multi-part folding lift surfaces designed to optimize long-range forward cruise while maintaining an ultra-compact ground footprint.

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Deployment Footprint

ZERO-FOOTPRINT VTOL

Zero-Footprint Vertical Takeoff and Landing (VTOL). Complete runway independence allowing rapid tactical deployment and cargo extraction from tight clearances, unpaved surfaces, and remote combat zones.

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Mission Classifications

DUAL-USE / UTV — UMV

Dual-use technology with military and commercial applications with cargo, multi-passenger (Ironbird/Sugarbird) and single passenger (IronBoard/SugarBoard) use cases.

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