Overview  

The ASIS - Airborne Surveilance and Intelligence System -  is a combination between the advantages of an unmanned system to manned air vehicle capabilities.

The ASIS consists of a light airplane which carries an EO/IR payload and Innocon's unique  ground control station.

Mission Capabilities

• Real-time surveillance

• Search and location of enemy forces

• Track of enemy movement

• Battlefield situation awareness

• Territory and installation security

• Wild life monitoring

• Forest fire detection

• Guidance of attack forces and battle field control.

• Involving the high command in tactical decisions.

• Targeting and coordinating attack on enemy force.

• Search and rescue

• Search for troops

• Coordinate rescue missions.

Advantage Over UAV Systems

• Rapid deployment, airborne observer can start performing a mission while GCS is deploying towards battle zone.

• Extremely low cost relative to UAV systems.

• Operate at low altitude under clouds if necessay and then climb back in order to transmit data to GCS.

• Wide angle view of the battle field by the airborne operator and pilot.

Airborne System Features

• Electro-optical payload, composed of two sensors (TV and FLIR) gimbaled and stabilized

 for day/night observation.

• Video and Data monitors for the airborne operator and pilot

• Mission Avionics for navigation and payload command & control.

• Data-link system for transmitting Video, Telemetry and Voice to the ground, and

 receiving commands and voice from the ground station to pilot, payload and avionics.

Ground Control System Features

• Mission Control Station, with option to be mounted in one of the following:

 • S-280 shelter.

 • Inside of a light truck.

 • base station.

 • Portable Receiving Stations.

• The main function of the MCS:

 • Payload control .

 • Mission Control.

 • Display and record video images.

 • Intelligence exploitation.

The Aircraft - P92-Echo super specification

Engine

Power max: 100 Hp (73.5 kW) @ 5800 rpm

Propeller: Hoffmann H017GHM-174 177C

Fuel: Euro Super or Unleaded

Tanks: 100L

Weight: Max T.O. 550 Kg ( 1212 lb )

Basic empty weight: 306 kg ( 705 lb )

Load ultimate factor: +3.8    -3

Performance

Max speed s/l: 235 km/h (127 KTS)

Cruising speed 75%: 210km/h (113 KTS)

Rate of climb: 6,0 m/sec (1180 ft/min)

Stalling speed (with flap): 64 Km/h ( 34 KTS )

Service ceiling: 4500 m (14800 ft )

Max range (without reserve) 65%: 800 Km ( 430nm )

Take off to 15m (50 ft): 245 m ( 800 ft )

Take off run: 140 m ( 459 ft )

Landing run: 100 m ( 328 ft )

Dimensions

Wing Span: 8,7 m (28.5 ft)

Length over-all: 6,4 m (21 ft)

Height over-all: 2.5 m (8.2 ft)

Width cabin: 1.14 m (44.8 inc)

Wing area: 13,2 mq (129 sq.ft.)

Wing Dihedral: 1,5°

Tail plane span: 2,9 m (9.5 ft)

Wheel track: 1,8 m (5.9 ft)

Wheel tires: 5,00-5