AEROSPACE DEFENSE & LOGISTICS
THE JETAYU
Hybrid-eVTOL Platform
Flight Profile Jetayu - MK4
Conventional Limitations
Energy & Endurance
Limited range and heavy battery constraints limit operational viability.
Operational Safety
Vulnerabilities resulting from exposed rotor blades and FOD hazards.
Acoustic Signature
High-frequency noise impacts stealth operations and urban use.
Systemic Inefficiency
Massive aerodynamic losses in traditional quadcopter airframes.
Jetayu Innovations
APU Regeneration
In-flight regeneration during the cruise phase to maximize endurance.
Propulsion Redundancy
Combined electric and fluidic systems ensure mission-critical redundancy in contested airspace.
Aero-Acoustics
Integrated acoustic liners and internal ducted architecture significantly reduce disc loading and tonal noise.
Adaptive Morphing
Morphing wings actively adjust and stow to eliminate vertical drag during VTOL flight phases.
Applications of JETAYU
Remote Lifting & Logistics
Precision slung-loading in rugged terrain. Capable of transporting pre-fab modules up to 150 KG payloads at 15,000 FT altitudes.
High-Altitude Logistics
Autonomous cargo delivery in low-density altitudes. Operating up to 18,000 FT in extreme cold (-4°C), supporting loads up to 150 KG.
Offshore Utility Support
Critical replacement part delivery to offshore oil and wind platforms, maintaining operational continuity. Max payload of 150 KG.
Disaster Relief Cargo Drops
Rapid deployment of essential aid post-catastrophe, air-dropping up to 150 KG of food, water, and medical supplies into inaccessible zones.
Subsystem Telemetry
Restricted Access
Engineering telemetry is classified. Enter clearance code.
ACCESS DENIED.
Internal Architecture
Complete technical schematic outlining the hybrid-eVTOL UAV cross-section.
Mixed-Flow Compressor
66,000 RPM titanium core for fluidic injection.
PA1 Propulsion Pods
Fluidic multipliers utilizing the Coanda effect.
Morphing Wings
Translating-pivot sequence for VTOL to high-lift.
Propeller Blade Design
Precision carbon fiber blades optimized for high-efficiency thrust and kinetic recovery.
Energy Core
16S Silicon-Anode pack with mid-flight kinetic regeneration via windmilling propellers.
Organization Details
Corporate Registry
COMPANY NAME
JC AEROSPACE PRIVATE LIMITED
DATE OF INCORPORATION
14/05/2026
CIN
U30300KA2026PTC220821
HEADQUARTERS
BENGALURU, KARNATAKA