GRS 6 600 SD Speedy 115m2
General description:
Use parachute:
| TYPES | 600 | 650 | ||
|---|---|---|---|---|
| Total safety coefficient of the canopy by ASTM F2316-12 | Test ASTM 1,5 | |||
| Allowed max. operational weight MTOW | Kg | 600 | 650 | |
| Allowed never exceed speed for use VNE | Km/h | 315 | 280 | |
| Maximum operational opening dynamic shock at VNE and MTOW | kN/G | 26,7 | 26,4 | |
| Tested total time of full canopy in VNE and MTOW | sec. | 5,6 | ||
| Overall time of full canopy stretching at the speed of 95 km/hod. at MTOW | sec. | 5,2 | ||
| Descending recorded at 1000m/AMSL Min. Max MTOW m/s Descending recorded at 1500m/AMSL |
m/s | 7,1-7,3 7,3-7,5 |
||
| Maximum load at speed 250 km/h | Kg | 750 | ||
| Maximum operational opening dynamic shock at the speed 250 Km/h | kN | 32,1 | ||
| Minimum projected rescue height for horizontal fly | m./km/h | 110/90 | ||
| Method ejection | Container Short sleeve | |||
| Canopy | ||||
| Area | m2 | 115 | ||
| Number of lines and panels | 26 | |||
| Nominal diameter | m | 10,6 | ||
| Quantity of slots/Slider* | 22 | |||
| Ballistic device | Rocket engine MK4 | |||
| Igniter – mechanical ignition | Dual primer | |||
| Stationary rocket engine pull | 670 N/sec. 68Kg | |||
| Maximum rocket engine pull | 930 N/sec. 94Kg | |||
| Ballistic and drawing device weight | 2.62Kg | |||
| Burn time (- 40°C – +60°C) | 1 sec. ± 0,2 sec. | |||
| Cycle Exchange 6 years | ||||
| Dimensions | ||||
| Dimensions B1-B13 in products | mm | B1-B14 | ||
| OUT/INr | mm ø |
— — |
||
| Weight unit – GRS | Kg | 11,5 | ||
| Drawing sling length weight |
m. Kg |
5,5 0,74 |
||
| IN/OUT # / Soft R + (0,75kg) |
Kg | — | ||
| Total weight±4% GRS Soft B GRS Soft B2 |
Kg | 12,3 | ||
SOFT
B1 …………. 165 x 250 x 540 mm
B2 …………. 190 x 250 x 490 mm
B3 …………. 150 x 270 x 540 mm
B4 …………. 220 x 235 x 410 mm
B5 …………. 180 x 240 x 500 mm
B6 …………. 150 x 260 x 570 mm
B7 …………. 245 x 195 x 560 mm
B8 …………. 240 x 240 x 400 mm
B9 …………. 180 x 270 x 440 mm
B10 ……….. 150 x 235 x 600 mm
B11 ……….. 160 x 330 x 420 mm
B12 ……….. 210 x 195 x 480 mm
B13 ……….. 140 x 270 x 480 mm
B14 ……….. 160 x 255 x 520 mm
B15 ……….. 190 x 250 x 420 mm
Certification:
According to ASTM F2316-12
According to Patent No.: US 7,997,535 B2
Date of Patent : Aug.16 2011
GRS 6/600 SD – 290
x= speed aircraft VNE – km/h
y= Dynamic opening shock – power kN
| curve 1 | 90 | 150 | 210 | 260 | speed km/h |
| 24,2 | 24,3 | 24,8 | 26,4 | power kN | |
| curve 2 | 90 | 150 | 280 | 315 | speed km/h |
| 22,6 | 22,6 | 23,5 | 26,7 | power kN | |
| tested | 250 | speed km/h | |||
| 33,0 | power kN |
ASTM F2316-12
Descending at 1500m AMSL
curve 1 – Use Max. 650 kg limit – 7,73 m/sec.
curve 2 – 600 kg – 7,43 m/sec.
tested – 750 kg – Test Max.
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