GRS 6 90-120 SD 25m2 UAV
General description:
Use parachute:
| TYPES | 90 | 90-120 | 90 | |
|---|---|---|---|---|
| Total safety coefficient of the canopy by ASTM F2316-12 | Test ASTM 1,5 | |||
| Allowed max. operational weight MTOW | Kg | 90 | 90-120 | 90 |
| Allowed never exceed speed for use VNE | Km/h | 410 | 290 | 250 |
| Maximum operational opening dynamic shock at VNE and MTOW | kN/G | 11,0 | 12,4-15,6 | 15,6 |
| Tested total time of full canopy in VNE and MTOW | sec. | 3,3 | 2,1 | 1,2 |
| Overall time of full canopy stretching at the speed of 95 km/hod. at MTOW | sec. km/h | 3,3/180 | 3,2/120 | 3,0 |
| Descending recorded at 1000m/AMSL Min. Max MTOW m/s Descending recorded at 1500m/AMSL | m/s | 6,0-6,9 --- | ||
| Maximum load at speed km/h | Kg | |||
| Maximum operational opening dynamic shock at the speed Km/h | kN | |||
| Minimum projected rescue height for horizontal fly | m./km/h | |||
| Method ejection | Container Short sleeve | |||
| Canopy | ||||
| Area | m2 | 25 | ||
| Number of lines and panels | 18 | |||
| Nominal diameter | m | 5,1 | ||
| Quantity of slots/Slider* | 3 | |||
| Ballistic device | Rocket engine 120 | |||
| Igniter – mechanical ignition | Dual primer | |||
| Stationary rocket engine pull | 480 N/sec. 49Kg | |||
| Maximum rocket engine pull | 750 N/sec. 76Kg | |||
| Ballistic and drawing device weight | 2.0Kg | |||
| Burn time (- 40°C - +60°C) | 1 sec. ± 0,2 sec. | |||
| Cycle Exchange 6 years | ||||
| Dimensions | ||||
| Dimensions B1-B13 in products | mm | |||
| OUT/INr | mm ø | | ||
| Weight unit - GRS | Kg | 3,4 | ||
| Drawing sling length weight | m. Kg | 4,0 0,4 | ||
| IN/OUT # / Soft R + (0,75kg) | Kg | |||
| Total weight±4% GRS Soft B GRS Soft B2 | Kg | 5,8 (including rocket) | ||
