| Parameter | Specification |
|---|---|
| Frame Type | Quadrotor – Carbon Composite |
| Flight Time | Up to 60 minutes (based on payload) |
| Payload Capacity | Up to 1 kg |
| Maximum Take-off Weight (MTOW) | 4 kg |
| Communication Range | Up to 15 km (HD encrypted link) |
| Flight Modes | Manual / GPS / Fully Autonomous |
| Navigation System | RTK GNSS + IMU Fusion |
| Power System | 15000 mAh Solid State Li-Ion |
| Camera Compatibility | EO/IR, RGB, Thermal, LRF, AI-based, 30x–180x Zoom |
| Operating Temperature | -20°C to +55°C |
| Wind Resistance | Up to 15 m/s |
| Applications | Surveillance, Reconnaissance, Target Locking, Border Patrol, Search & Rescue, Night Operations, Threat Detection |
| Parameter | Specification |
|---|---|
| Long Endurance Tactical Surveillance | Up to 3 Hours Flight Duration |
| Extended Area Monitoring | Operational Range up to 50 km |
| Runway Independent Operations | VTOL Fixed Wing UAV |
| Efficient Hybrid Flight | 4 + 1 Configuration (4 Lift Motors + 1 Cruise Motor) |
| Large Area Coverage & Stable Flight | 2500 mm Wingspan Fixed Wing Platform |
| Low Logistics & Silent Operations | Battery Operated Electric Propulsion System |
| Border & Tactical Reconnaissance | Optimized for Defence Surveillance & Suitable for ISR Missions |
| Target Distance Measurement | Laser Range Finder (LRF) Payload Support |
| Day Surveillance Missions | High Resolution EO Camera Payload |
| Night & Low Visibility Surveillance | Thermal / Infrared Camera Payload |
| Long Range Visual Observation | High Zoom Stabilized EO/IR Gimbal Payload |
| Autonomous Mission Capability | Waypoint Navigation & Autonomous Flight Modes |
| Real-Time Intelligence Gathering | Live Video & Telemetry Transmission to GCS |
| Secure Tactical Communication | Encrypted Data Link Communication System |
| Operations in Difficult Terrain | Suitable for Mountains, Border Areas, Forest & Desert Operations |
| Rapid Field Deployment | Portable System with Quick Deployment Capability |
| Fail Safe Operations | Auto Return-To-Launch, Fail Safe Landing & Mission Recovery |
| Intelligence, Surveillance & Reconnaissance (ISR) | Multi-Sensor Payload Integration Capability |
| Primary role | Training / Basic | Surveillance / Kamikaze / Payload dropping | Long-range Surveillance / Ammunition & payload |
|---|---|---|---|
| MTOW | 3.0 kg (USER) | 6.0 kg (USER) | 12.0 kg (USER) |
| Max payload | 0.8 kg (USER) | 2.0 kg (USER) | 5.0 kg (USER) |
| Typical payloads | Small EO/IR camera, beacon, simple comms | EO/IR gimbal, telemetry, small warhead (kamikaze config) | Large EO/IR, multiple cargo/munition dispensers, long-range comms |
| Airframe type | Small high-wing fixed wing, foam/carbon composite | High-wing composite | Twin-boom / conventional long-endurance |
| Powerplant | Electric brushless motor, direct-drive prop | Electric brushless motor, efficient prop | Hybrid option (gasoline + electric) or heavy electric motor (recommended hybrid) (EST) |
| Battery / fuel | 3S Solid State Li-Ion Battery | 6S Solid State Li-Ion Battery | 12S Solid State Li-Ion Battery |
| Cruise speed | 50–65 km/h (EST) | 70–85 km/h (EST) | 85–110 km/h (EST) |
| Max speed | 90 km/h (EST) | 100 km/h (USER) | 130 km/h (EST) |
| Endurance (typical) | 1 hour | 1 hour | 3 hour |
| Range | 10 km | 10 km | 20 km |
| Service ceiling | 3,000 m ASL (EST) | 4,000 m ASL (EST) | 5,000 m ASL (EST) |
| Launch / recovery | Hand-launch + Belly Landing | Hand-launch + Belly Landing | Catapult / runway / arrested recovery / parachute (EST) |
| Comms | 2.4 GHz telemetry (short LOS) (EST) | 2.4 GHz telemetry (short LOS) (EST) | 2.4 GHz telemetry (short LOS) (EST) |
| Materials | Foam + carbon spars / composite | Foam + carbon spars / composite | Carbon composite / advanced composites |
| Ground control | PC/Tablet GCS, basic telemetry | PC/Tablet GCS, basic telemetry | Full mission GCS, multi-aircraft control, encrypted link (EST) |
| Safety | Failsafe RTL (EST), low-battery return | Failsafe RTL, low-battery return (EST) | Redundant avionics, parachute/airbag options, encrypted control |
| Typical ops | -10°C to +45°C (EST) | -15°C to +50°C (EST) | -20°C to +50°C |
| Specification | VIRAAT S | VIRAAT M | VIRAAT L |
|---|---|---|---|
| Role / Type | VTOL cargo drone (quad-tilt / quadrotor) | VTOL hybrid cargo (octo / quadplane) | Hybrid VTOL cargo (quadplane / tilt-truss) |
| Payload capacity (useable) | 20 kg | 40 kg | 80 kg |
| Empty weight (airframe + avionics) | ~30 kg | ~55 kg | ~110 kg |
| Maximum takeoff weight (MTOW) | ~60 kg | ~120 kg | ~240 kg |
| Typical endurance (full mission, cruise) | 45 Minutes | 30 Minutes | 30 Minutes |
| Typical operational radio range (line-of-sight / BVLOS) | 20 km | 20 km | 40 km |
| Cruise speed | 80 km/h | 90 km/h | 100 km/h |
| Max speed | 60 km/h | 80 km/h | 80 km/h |
| Service ceiling | 3,000 m | 3,000 m | 4,000 m |
| Propulsion | Electric VTOL (high power Li-ion packs) | Electric VTOL (high power Li-ion packs) | Electric VTOL (high power Li-ion packs) |
| Powerplant / energy | Li-ion battery (modular packs) | Li-ion battery (modular packs) | Li-ion battery (modular packs) |
| Flight controllers / autonomy | Dual redundant FC; advanced mission profiles | Dual redundant FC; advanced mission profiles | Triple-redundant FC; full-mission autopilot |
| GNSS / navigation | GPS + GLONASS + IMU | Multi-GNSS + RTK capable + IMU | Multi-GNSS + RTK/INS seamless navigation |
| Parameter | Specification |
|---|---|
| Role | Tactical FPV recon, secure low-latency comms, precision non-lethal drops |
| Payload | Up to 5 kg (modular pods) |
| Airframe | Compact carbon-composite; quick-swap payload rails |
| Weight | Empty 1 kg; MTOW 2–3 kg |
| Propulsion | Electric — modular Li-Ion / Li-Po packs |
| Endurance | 20–60 minutes (depends on payload & mode) |
| Cruise / Max speed | Cruise 60–120 km/h; Max 150+ km/h |
| FPV link | Digital and Analogue HD low-latency (<50 ms) + analogue fallback |
| Camera / Gimbal | 2–3 axis stabilized EO HD; optional low-light / IR |
| Navigation | Multi-GNSS + IMU; optional RTK & visual-odometry |
| Autonomy | Manual FPV, Assisted, Waypoints, Precision loiter, RTH |
| Security | AES-256 encrypted datalink; tamper-evident mission logs |
| Optical-fibre option | Removable tether (reel/spool) for ultra-low-latency secure feed |
| Payload interfaces | 12–28V power, CAN, UART (RS232), Ethernet (higher-end pods) |
| Payload power | 50–200 W continuous (config dependent) |
| Launch / Recovery | VTOL launch; parachute or net recovery options |
| Safety features | Geofence, auto-land on failsafe, parachute/net recovery |
| Environment | Operates ~ −10°C to +45°C (hardened variants available) |
| Maintenance | Modular batteries; quick-swap motors/ESCs; common avionics stack |
| Compliance | Designed for lawful, non-lethal ops — follow local regs/ROE |
| Parameter | Specification |
|---|---|
| Frame Type | Quadrotor – Carbon Composite |
| Flight Time | 60 minutes (depending on payload) |
| Payload Capacity | Up to 3 kg |
| Maximum Take-off Weight (MTOW) | 8 kg |
| Communication Range | Up to 15 km (HD encrypted link) |
| Flight Modes | Manual / GPS / Fully Autonomous |
| Navigation System | RTK GNSS + IMU Fusion |
| Power System | 21000mAh Solid State Li-Ion |
| Camera Compatibility | LiDAR, EO/IR, RGB, Thermal, LRF, AI-based, 30x–180x Zoom |
| Operating Temperature | -20°C to +55°C |
| Wind Resistance | Up to 15 m/s |
| Applications | Payload Dropping, Surveillance, Reconnaissance, Target Locking, Border Patrol, Search & Rescue, Night Operations, Threat Detection |
