GRS 6 1750-1950 SDS/FF 360m2





Use parachute:

TYPES 1750 1950
Total safety coefficient of the canopy by ASTM F2316-12 Test ASTM 1,5
Allowed max. operational weight MTOW Kg 1750 1950
Allowed never exceed speed for use VNE Km/h 390 350
Maximum operational opening dynamic shock at VNE and MTOW kN/G 55,7/3,2 59,5/3,1
Tested total time of full canopy in VNE and MTOW sec. 6,2
Overall time of full canopy stretching at the speed of 95 km/hod. at MTOW sec. 6,5
Descending recorded at 1000m/AMSL
Min. Max MTOW m/s
Descending recorded at 1500m/AMSL
m/s 7,0-7,3
7,2-7,5
Maximum load at speed 250 km/h Kg 2400
Maximum operational opening dynamic shock at the speed 250 Km/h kN 58
Minimum projected rescue height for horizontal fly m. 170
Method ejection
Short sleeve
Canopy
Area m2 360
Number of lines and panels
64
Nominal diameter m 19,2
Quantity of slots/Slider*
256*
Ballistic device
Rocket engine 322
Igniter – mechanical ignition
Dual primer
Stationary rocket engine pull
1320 N/sec. 134Kg
Maximum rocket engine pull
1850 N/sec. 189Kg
Ballistic and drawing device weight
3.22Kg
Burn time (- 40°C - +60°C)
0,95 sec. ± 0,2 sec.
Cycle Exchange 6 years
Dimensions
Soft pack
B1-LxWxD
B2-LxWxD
cm
cm
68x40x30
Weight unit - GRS
Drawing sling
length
weight
m.
Kg
4x 6
1,5
Total weight±4%
GRS Soft B
GRS Soft B2
Kg ---
45,0

Tested according to new methodology
#
#

x= Speed aircraft VNE - km/h
y= Dynamic opening shock - power kN

curve 1 150 220 320 390 speed km/h
47,0 48,3 50,2 55,7 power kN
curve 2 150 200 290 350 speed km/h
45,0 46,4 50,0 59,5 power kN


curve 1 - 1750 kg
curve 2 - 1950 kg

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