Apollo
Apollo is a compact quadplane VTOL designed to combine vertical take-off and landing with the range and cruise efficiency of a fixed-wing platform. With a 1.61 m wingspan, 6.1 kg airframe weight and up to 1 kg payload capacity, it cruises at 22 m/s and delivers up to 35–40 km range and 40 minutes of endurance without payload. Its stabilized dual-light imaging payload combines a 5 MP visible sensor with 384 × 288 thermal imaging, 4× digital zoom, RTSP video streaming, onboard recording and intelligent target tracking. GNSS navigation and ground telemetry over TCP/UDP support real-time mission monitoring across ISR, survey, mapping, surveillance and observation missions.
Published specifications.
Performance figures are dependent on payload, operating conditions and mission configuration.
Related platforms.
In developmentEagle Eye
Lightweight mid-range fixed-wing UAV for tactical reconnaissance and survey missions. Composite or laser-cut balsa airframe, battery-electric propulsion, ArduPilot autopilot with Auto / Loiter / Stabilize / RTL flight modes. RF-primary comms with optional GPS telemetry.
In productionIcarus II
Production-tuned variant of the Icarus composite VTOL, sharing its CF/FG airframe and ArduPilot autopilot. Configurable electric or IC-engine propulsion, ARF kit assembly. 50–60 min endurance, 60–80 km operational range on a single charge, GPS-primary comms with RF backup.
In productionIcarus
Composite VTOL platform for long-range ISR, mapping, and surveillance missions. Built on a carbon-fibre / fibreglass airframe with ArduPilot-based autopilot and configurable electric or IC-engine propulsion. Shipped as an ARF kit; GPS comms with RF fallback.