Type
Small arms target.
Development
Designed as all-arms air defence target for use with small arms and machine guns. Also used as basic trainer for operators of the larger and faster Baaz (which see).
Airframe
Small, simple high-wing monoplane with GFRP fuselage and a polystyrene foam, epoxy laminated wing. Full span flaperons and elevator; no rudder. Current models have increased fin area and less tapered wings. No landing gear.
Mission payloads
Cannot carry mission pay load
Guidance and control
Radio command (four-channel VHF transceiver). Transmitter power 9.6 V at 1.2 Ah; RF output 1 W. Receiver power 6 V at 1.2 Ah. Rechargeable battery. Ground support equipment consists of a box containing a 2.5 litre (0.66 US gallon; 0.55 Imp gallon) fuel container, electric engine starter, ammeter, 12 V battery to power equipment, and a selection of hand tools.
Launch
Hand-launched
Recovery
Belly landing on any reasonably level terrain
Operational status
In production and service
Customers
Royal Saudi Air Force & Pakistan Armed Forces
Specifications
Power plant
One 0.9 kW (1.2 hp) 10 cc glow-fuel engine with two-blade propeller. Fuel capacity 0.38 litre (0.10 US gallon; 0.08 Imp gallon).
Dimensions
Wing span 1.60 m (5 ft 3.0 in)
Length overall 1.41 m (4 ft 7.5 in)
Tailplane span 0.60 m (1 ft 11.6 in)
Weights
Max launching weight 2.8 kg (6.2 lb)
Performance
Max level speed 75 kt (140 km/h; 87 mph)
Endurance 20 min
Prime contractor
Pakistan Aeronautical Complex (PAC), Aircraft Manufacturing Factory Kamra.