Rescue systems for aircraft, balloons, helicopters and gyroplanes - RESCUE SYSTEMS FOR AIRCRAFT

Magnum 250

Technical d​ata

Name Unit Value
Maximum permitted load kg 300
Maximum speed km/h 150
Rescue system weight
(including rocket, without activation line)
kg 8
Dimensions
(lxwxh)
mm Ø185+60x455
Opening time at maximum speed s 3
Minimum safe deployment altitude
(AGL) during horizontal flight
m / km/h 80 / 60
Maximum overload
(with maximum load)
kN 15
Descent
(with maximum load)
m/s 7
Sleider   no
Container type   duralumin
Canopy    
Area 65
Repack interval year 5
Ballistic device    
Rocket engine type   Magnum 450
Total impulse at 20°C kNS 0,303
Activation   Mechanical
Burn time at 20°C in second s 0,57 ± 0,03
Certified by   DULV

Download the manual HERE.

 

 

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