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CHACAL 2

Product catalog summary

Overview: The CHACAL 2 is a stealth UAV developed by ALCORE Technologies SA, designed for high-performance aeronautical applications. It is primarily used for tactical reconnaissance, surveillance, target acquisition, aerosonde, and missile simulation.

Specifications:

Dimensions: Span: 2.60m, Length: 3.00m, Height: 0.67m
Weight: Operational: 75kg, Max Takeoff: 85kg, Payload: 10kg, Bulk Payload Volume: 15 liters
Power Plant: Two-stroke gasoline engine with four cylinders, 24 hp carbon propeller, or turbojet 60 lb (27kg)
Batteries: Cad/nickel for ignition

Performance:

Speed: Max: 280 km/h, Loiter: 100 km/h, Cruise: 260 km/h
Climb Ratio: 4 m/s
Altitude: Ceiling: 0m to 1500m, Service: 300m to 1000m
Endurance: 3 hours
Range: 700 km without wind

Payload: Equipped with CCD and ILL on 2-axis gimbal joints, digital data link, and a mission radius of 50 km tested.

Guidance and Control: Features include a 3-axis autopilot, glide mode, GPS, automatic flight, and pre-programmed missions.

Ground Station: Portable ground station using a micro-computer with WinNT, derived from tactical UAV software, for mission preparation, tracking, and image visualization.

Launch and Recovery: Utilizes a Sandow launcher for piloted flights and a pneumatic catapult for automatic launches.

Weather Restrictions: Tested in drizzle, pouring rain, and wind up to 10 m/s. Snow conditions are yet to be tested. Operates in temperatures from -10 to +50 degrees Celsius.

Program Status: Developed from 1989 to 1992, with production starting in 1993/94. Used for training exercises since 1994, with no crashes reported since the first flight.

Additional Information: The CHACAL 2 was tested in 1992 by DASSAULT ELECTRONIC for radar calibration training exercises.

Catalog excerpts

ALCORE Technologies SA www.alcore-tech.com Description: furtive UAV with hight aeronautique performances. System application : tactical reconnaissance and surveillance, target acquisition, aerosonde, missile simulation. Description : Vecteur aérien dont les performances aéronautiques sont très importantes Application du système : Reconnaissance et surveillance tactique ; acquisition de la cible ; aérosonde ; simulation missile. Data Platform Span Length Height Operational weight Included payload Max Takeoff Weight Stand-by potential Bulk payload Data Vecteur aérien Envergure Longueur Hauteur Poids opérationnel Dont charge utile Potentiel max. Réserve de potentiel Volume charge utile Power plant Groupe Moto Propulseur Moteur two-stroke gasoline engine four cylinders 24 hp carbon propeller; or turbojet 60 lb (27kg). Batteries Cad/nickel for ignition Cad/nickel pour l’allumage Control Electronic control Contrôleur électronique Performance Max speed Loiter speed Cruise speed Climb ratio Ceiling Service altitude Glide performance Max endurance Run following distance Performances Vitesse max. Vitesse mini Vitesse de croisière Taux de montée Altitude Hauteur de vol Finesse max. Endurance Distance parcourue sans vent Payload CCD on 2 axes Cardan joint piloted ILL on 2 axes Cardan joint piloted Data link Mission radius Charge utile CCD ILL Transmissions Portée CCD sur cardan 2 axes pilotés ILL sur cardan 2 axes pilotés numérique 50km testé ALCORE Technologies SA www.alcore-tech.com

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ALCORE Technologies SA www, a!core-tech, com infoCa a!core-tech, com

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