| Variant | |
| Role |
battlefield reconnaissance
target positioning and illumination
communication relay
battle damage assessment
|
| Country | |
| Builder | North Industries Corporation |
| First Flight | |
| Status | |
| Number built | |
| Operators | |
| Cost | |
| Comparable Aircraft | |
| Recognition | |
| Ritir span | meters | feet |
| Fuselage Maximum Diameter | meters | feet |
| length | meters | feet |
| height | meters | feet |
| Weight empty | kg | lb |
| takeoff (clean) | kg | lb |
| takeoff (maximum) | 500 kg | lb |
| Fuel, Internal | kg | lb |
| Fuel, External | kg | lb |
| Payload | 150 kg | lb |
| Max weapon load | kg | lb |
| Armament |
up to 8 Blue Arrow 5 missiles
up to 8 Red Arrow 12 missiles
|
| Power Plant | |
| Thrust, max, SLS, ISA | x kg | x lbst |
| Internal fuel (usable) | kg | lb |
| Performance (clean, ISA) | |
| cruising speed | 90 km/h |
| Max level speed (sea level) | 140 km/h |
| Limit speed | KEAS / MN |
| Stall speed (landing, 20% fuel) | 90 KCAS |
| Stall speed (reference) | KCAS |
| Rate of climb (SL) | feet/min |
| Service ceiling | 4000 meters | feet |
| maximum take-off altitude | 3000 meters | feet |
| control radius | 150 kilometers | miles |
| endurance | 5 hours at full load
|
| Range, clean | km | nm |
| Max sustained Load Factor (S.L.) | g |
| Max sustained Load Factor (15,000 feet) | g |
| Max sustained Turn Rate (15,000 feet) | deg/sec |
| Takeoff ground run (S.L.) | meters | feet |
| Landing ground roll (S.L., 20% internal fuel) | meters | feet |
| Limit Load factor | + g / - g |
| Crew, air | - 0 - |
| Crew, ground | ? |
