OBSERVER-121

  • Easy to operate and carry

    Tailored for single human carry and direct hand-launch from the spot. Landing can be performed via stalled landing or through the integrated parachute mechanism.

  • Lightweight

    Designed for rapid deployment and high mobility for several commercial applications of low-altitude intelligence, surveillance, and reconnaissance (ISR).

  • Autonomous missions

    Can be operated manually or programmed for autonomous operation, utilizing the system's advanced avionics and precise GPS navigation.

  • Harsh Environment

    Reliable to fly in harsh environments such as heavy wind and rain. High impact resistance to make it fully recoverable in complex environment conditions.

OPERATIONAL CHARACTERISTICS

Payload: Camera and gimbal up to 700g

Launch Method: Hand-Lauched

Recovery Method: Landing / Parachute.

KEY FEATURES

Small Size and Lightweight

Fused materials structure

Easy to Carry

Easy to Operate

Autonomous Navigation

Reliable use in Harsh Environment

Realtime Situational Awareness

 

TECHNICAL CHARACTERISTICS

Max. Take-off Weight: 5500g

Endurance: 60-90 min

Speed: 35-70 km/h

Wing-Span: 1960mm

Length: 1070 mm

Heavy Duty Case

Downlink imagery from HD camera and navigation path

Herelink Ground Control Station

 

FLYING BEYOND LIMITS.