Pakistan's UAS Sensing Δ 14th of January 2014 Ω 2:43 AM

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«UAS Sensing	Θ	Θ
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~ Pakistan Aeronautical Complex

»Pakistan Aeronautical Complex

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~ ABABEEL AERIAL DRONE

»ABABEEL AERIAL DRONE

Type
ξ Small arms target
Development
ξ Designed as all-arms air defence target for use with small arms and machine guns.
ξ Also used as basic trainer for operators of the larger and faster Baaz (which see).

Airframe
ξ Small, simple high-wing monoplane with GFRP fuselage and a polystyrene foam, epoxy laminated wing.
ξ Full span flaperons and elevator; no rudder.
ξ Current models have increased fin area and less tapered wings.
ξ No landing gear.

Mission payloads
ξ Cannot carry mission pay load

Guidance and control
ξ Radio command (four-channel VHF transceiver).
ξ Transmitter power 9.6 V at 1.2 Ah;
ξ RF output 1 W.
ξ Receiver power 6 V at 1.2 Ah.
ξ Rechargeable battery.
ξ Ground support equipment consists of a box containing a 2.5 litre (0.66 US gallon; 0.55 Imp gallon) fuel container,
ξ electric engine starter, ammeter, 12 V battery to power equipment, and a selection of hand tools.

Launch
ξ Hand-launched

Recovery
ξ Belly landing on any reasonably level terrain

Operational status
ξ In production and service

Customers
ξ Royal Saudi Air Force
ξ Pakistan Armed Forces
Specifications

Power plant
ξ One 0.9 kW (1.2 hp) 10 cc glow-fuel engine with two-blade propeller.
ξ Fuel capacity 0.38 litre (0.10 US gallon; 0.08 Imp gallon).

Dimensions
ξ Wing span 1.60 m (5 ft 3.0 in)
ξ Length overall 1.41 m (4 ft 7.5 in)
ξ Tailplane span 0.60 m (1 ft 11.6 in)

Weights
ξ Max launching weight 2.8 kg (6.2 lb)

Performance
ξ Max level speed 75 kt (140 km/h; 87 mph)
ξ Endurance 20 min

Prime contractor
ξ Pakistan Aeronautical Complex (PAC), Aircraft Manufacturing Factory Kamra.

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~ BAAZ AERIAL DRONE

»BAAZ AERIAL DRONE

Type
ξ Recoverable aerial target.

Development
ξ Designed for use with air defence guns and short-range SAM systems;
ξ system includes optical tracking facilities.

Airframe
ξ Simple high-wing monoplane, with parallel chord wings and horizontal tail;
ξ GFRP fuselage,
ξ epoxy laminated polystyrene wing.
ξ No landing gear.

Mission payloads
ξ Cannot carry mission pay load

Guidance and control
ξ Radio command, by seven-channel VHF/FM transceiver.
ξ Transmitter power 9.6 V at 1.2 Ah;
ξ RF output 1 W;
ξ rechargeable battery.
ξ Receiver power 6 V at 1.2 Ah;
ξ rechargeable battery.
ξ Transceiver has two built in fail safe devices.
ξ If transmitter fails, engine shuts down after 1.5 seconds;
ξ if power fails or receiver malfunctions for any reason, including projectile strikes,
ξ an independent auxiliary power supply automatically operates the same fail-safe sequence.

Launch
ξ By bungee powered catapult.
ξ Set up time 20 minutes;
ξ turnaround time 5 to 10 minutes

Recovery
ξ Direct landing on reinforced belly, or parachute retrieval

Operational status
ξ In production and service

Customers
ξ Royal Saudi Air Force
ξ Pakistan Armed Forces

Specifications

Power plant
ξ One 100 cc (British Origin) two stroke engine with electronic ignition;
ξ two blade propeller
ξ Fuel is 20:1 petrol/oil mixture.

Dimensions
ξ Wing span 2.44 m (8 ft 0.0 in)
ξ Length overall 2.10 m (6 ft 10.7 in)

Weights
ξ Max launching weight 19 kg (41.9 lb)

Performance
ξ Max level speed 113 kt (209 km/h; 130 mph)
ξ Max range: visual 1.1 n miles (2 km; 1.2 miles)
ξ Optical 1.9 n miles (3.5 km; 2.2 miles)
ξ Max endurance 35 min

Prime contractor
ξ Pakistan Aeronautical Complex (PAC), Aircraft Manufacturing Factory Kamra.

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