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VihangX-1 — Fixed-Wing VTOL Hybrid — BVLOS UAS Delivery

VihangX-1: Fixed-Wing VTOL Hybrid BVLOS UAS Delivery, Built for Distance

VihangX-1 fixed-wing VTOL hybrid platforms combine vertical takeoff, efficient cruise flight and precision navigation for long-range autonomous delivery missions.

Designed for logistics, emergency supply, healthcare delivery, defence support and remote-area connectivity.

Engine Drives Generator
Electric Motors Power Rotors
Turbo Shaft Engine
VTOL & Forward Thruster
GPS Denied Operations
ZFW Not Exceeding 300 Kgs
Range
10 – 300 km
Payload
2 – 30 kg
Altitude
Beyond 20,000 ft
Mode
VTOL + Fixed-Wing Cruise
Data Logging
Onboard FDR
Navigation
Great Ellipse — Patent Pending
VihangX-1 fixed-wing VTOL hybrid delivery aircraft flying a BVLOS UAS route over a valley

Hybrid-electric drive — the engine drives a small generator; rotors are driven by electric motors.

IC engine type — turbo shaft engine.

Why a turbo shaft engine?

  • Reciprocating IC engines do not operate efficiently at high altitude due to lack of oxygen in the atmosphere.
  • Supports the requirement of operating the aircraft in sub-zero temperatures.

VTOL equipment & forward thruster — driven by electric propulsion.

Operates in GPS-denied environments — Great Ellipse Navigation.

ZFW (zero fuel weight) not exceeding 300 kg — batteries are heavy.

Other BVLOS UAS platforms
VihangX-2 — Fixed-Wing VTOL — Pure IC Engine

VihangX-2: Pure IC Engine VTOL Aircraft for Long-Range BVLOS UAS Delivery

VihangX-2 fixed-wing VTOL aircraft combines vertical takeoff, long-range cruise efficiency and IC-engine endurance for autonomous delivery missions beyond visual line of sight.

Designed for logistics, healthcare supply, emergency response, defence support and remote-area connectivity.

Pure IC Endurance. VTOL Flexibility. BVLOS Mission Reach.
VTOL Takeoff & Landing
Pure IC Engine Endurance
Fixed-Wing Cruise Efficiency
Payload Delivery Ready
Range
50 – 300 km
Payload
2 – 50 kg
Altitude
Beyond 20,000 ft
Power
Pure IC Engine
Data Logging
Onboard FDR
Navigation
Great Ellipse — Patent Pending
VihangX-2 fixed-wing VTOL pure IC engine aircraft flying a BVLOS UAS delivery corridor at sunset

Rotors — driven directly by the IC engine.

IC engine type — turbo shaft engine.

Why a turbo shaft engine?

  • Reciprocating IC engines do not operate efficiently at high altitude due to lack of oxygen in the atmosphere.
  • Supports the requirement of operating the aircraft in sub-zero temperatures.

VTOL equipment.

Operates in GPS-denied environments.

ZFW (zero fuel weight) not exceeding 200 kg.

Other BVLOS UAS platforms
VihangX-3 — LR-STD — Long Range · Short Takeoff · Delivery

VihangX-3: LR-STD Reciprocating Piston Engine Aircraft for Long-Range BVLOS Missions

VihangX LR-STD combines long-range cruise efficiency, short-takeoff flexibility, pure IC endurance and payload-ready architecture for autonomous BVLOS UAS delivery, surveillance and mission operations.

Built for logistics, healthcare supply, emergency response, defence support, industrial delivery, target tracking and remote-area connectivity.

Long Range. Short Takeoff. Delivery Ready.
Long-Range Capability — 430–540 nm
Short-Takeoff Flexibility
Pure IC Engine Endurance
Payload Delivery Ready
EO / IR + AI Mission Payloads
SATCOM & Mission Communications
Range
430 – 540 nm
Max Speed
≥ 100 kts
Transit Speed
≥ 80 kts
Cruise Speed
≤ 40 kts
MTOW
160 kg
ZFW
95 kg
Fuel
100 Octane Petrol
Data Logging
Onboard FDR
VihangX-3 LR-STD fixed-wing unmanned aircraft with pusher propeller cruising over a river valley

IC engine — reciprocating piston engine, made in India, running on 100 octane petrol. Pure IC propulsion with rear pusher propeller.

High-resolution EO / IR camera with on-board AI-powered object detection, identification and tracking software.

Full-Motion Video analysis support for identifying and tracking stationary and moving targets.

GoI-approved high-data-rate SATCOM for communication and data transfer.

Provision for ESM, lightweight radar and communication relay set as mission-fit payloads.

Other BVLOS UAS platforms
VihangX-4 — LR-STD Turbine Engine — Long Range · Short Takeoff · Delivery

VihangX-4: LR-STD Turbine Engine Aircraft for Long-Range BVLOS Missions

VihangX LR-STD Turbine Engine combines long-range cruise efficiency, short-takeoff flexibility, turbine-powered endurance and payload-ready architecture for autonomous BVLOS UAS delivery, surveillance and mission operations.

Built for logistics, healthcare supply, emergency response, defence support, industrial delivery, target tracking and remote-area connectivity.

Long Range. Short Takeoff. Mission Ready.
Long-Range Capability — 430–540 nm
Short-Takeoff Flexibility
Turbine Engine Endurance
Payload Delivery Ready
EO / IR + AI Mission Payloads
SATCOM & Mission Communications
Range
430 – 540 nm
Max Speed
400 kts
Cruise Speed
350 kts
MTOW
280 kg
ZFW
120 kg
Fuel
Jet A1
Data Logging
Onboard FDR
VihangX-4 LR-STD turbine engine unmanned aircraft with twin jet nozzles cruising over mountains at sunset

Turbine engine propulsion running on Jet A1 — turbine-powered long-range platform.

High-resolution EO / IR camera with on-board AI-powered object detection, identification and tracking software.

Full-Motion Video analysis support for identifying and tracking stationary and moving targets.

GoI-approved high-data-rate SATCOM for communication and data transfer.

Provision for ESM, lightweight radar and communication relay set as mission-fit payloads.

Other BVLOS UAS platforms
VihangX-5 — Blended-Wing Fixed-Wing UAV — ISR · Reconnaissance · R&D

VihangX-5: Blended-Wing Fixed-Wing UAV for ISR & BVLOS UAS Reconnaissance

A compact, rugged and field-deployable aircraft platform built for intelligence, surveillance, reconnaissance, target practice, R&D validation and tactical BVLOS UAS operations.

Designed for long-range mission testing, autonomous flight development, payload integration, reconnaissance training and field operations without heavy infrastructure.

Compact. Rugged. BVLOS UAS Ready.
160 nm Mission Range
FL240 Service Ceiling — 24,000 ft AMSL
Modular Payload Bay — 8 kg Runway / 2.5 kg VTOL
VihangX Flight Controller
Range
160 nm
Service Ceiling
FL240 / 24,000 ft
MTOW
51 kg
Payload
8 kg RW / 2.5 kg VTOL
Telemetry
30 km
Wingspan
3.5 m
Length
3 m
Height
1.2 m
Navigation
Great Ellipse Navigation
VihangX-5 blended-wing fixed-wing UAV with twin tail booms cruising above clouds at sunset

Blended flying wedge airframe — tapered wing profile, standard empennage, rear pusher propulsion, retractable landing gear.

VihangX flight controller with Great Ellipse Navigation and encrypted link options.

Runway takeoff and landing — field deployment without a hangar; detachable wings for transport.

Other BVLOS UAS platforms
No 332, 1st Floor, 6th Main Road, TK Layout, Saraswathipuram, Mysore — 570009, Karnataka contact@vihangx.com  ·  © 2026 VihangX