Техническа информация за Запасни парашути GRS
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Запасни парашути за DRON MULTICOPTER UAV
For videos and detailed information click on the product name.
TYPES |
GBS 10/30
|
GBS 10/50
|
GBS 10/150
|
GBS 10/350
|
GBS 10/350
|
GBS 10/650
|
GBS 10/650
|
||
|---|---|---|---|---|---|---|---|---|---|
Weight of ballistic rescue system GBS 10 |
g | 250 | 275 | 405 | 725 | 770 | 1400 | 1500 | |
Recommended operating weight UAV |
Kg | 3 | 5 | 5-15 | 15-35 | 15-35 | 35-65 | 35-65 | |
Allowed never exceed speed for use (VNE) Slider* |
Km/h | 80 | 80 | 80 | 80 | 220-300 | 90 | 220-320 | |
time of canopy opening (+0,5s to full filling chute) |
sec. | 0,5 | 0,5 | 0,5 | 0,8 | 1,0-2,0 | 1,2 | 1,5-2,5 | |
Height of rescue |
m | 5 | 5 | 5 | 8 | 30 | 15 | 50 | |
Descending |
m/s | 3,7-6,1 | 3,7-6,1 | 3,7-6,1 | 3,7-6,1 | 3,7-6,1 | 3,6-6,0 | 3,6-6,0 | |
Impact energy |
J | up to 75 | up to 130 | 35-380 | 100-680 | 100-680 | 230-1170 | 230-1170 | |
Method ejection |
Ballistic device | Ballistic device | Ballistic device | Ballistic device | Ballistic device | Ballistic device | Ballistic device | ||
tested by |
VUT Brno VZLÚ Praha |
Yes Yes |
Yes Yes |
Yes Yes |
Yes Yes |
Yes Yes |
Yes Yes |
Yes Yes |
|
Canopy |
|||||||||
| Number of lines and panels | 7 | 7 | 7 | 14 | 14 | 14 | 14 | ||
| Nominal diameter | m | 1 | 1,3 | 2 | 3 | 3 | 4,1 | 4,1 | |
| The central cord | Yes | Yes | Yes | Yes | No | Yes | No | ||
| Slider | No | No | No | No | Yes | No | Yes | ||
| Ballistic device | |||||||||
| Activator | pyrogenerator | pyrogenerator | pyrogenerator | pyrogenerator | pyrogenerator | iniciator | iniciator | ||
| Operating temperature | -20°C až +40°C | ||||||||
| Dimensions | mm | ø100 x 70 | ø100 x 80 | ø100 x 110 | ø100 x 190 | ø100 x 190 | 3 L | 3 L | |
Запасни парашути за Multicopter Drones Motoparaglider Trikes Ultralight GYRO
For videos and detailed information click on the product name.
| TYPES | GBS 10 Multicopter | GRS 2 110 GP-2S 28m2 |
GRS 2 140 GP-3S 32m2 |
GRS 2 160 GP-36S 36m2 |
GRS 3 180 GP-40S 40m2 |
GRS 3 270 60m2 | GRS 3 350 70m2 | GRS 3 450 92m2 | GRS 3 450 100 m2 GYRO |
|
|---|---|---|---|---|---|---|---|---|---|---|
| tested by Total safety coefficient of the canopy by ASTM F2316-12 |
BUT Brno | LAA ČR ZP-002/91 | by ZS-2 LAA ČR ZP-003/91 | by ZS-2 LAA ČR ZP-003/91 | by ZS-2 LAAČR | by ZS-2 LAAČR ULL-33/94 | by ZS-2 LAAČR ULL-05/94 | LAAČR ULL-04/94 | Test ASTM 1,5 | |
| Allowed max. operational weight (MTOW) | Kg | 0-35 |
65-110 | 100-140 | 120-160 | 180-190 | 270 270 |
350 350 |
450 475 475 |
560 |
| Allowed never exceed speed for use (VNE) | Km/h | 80-320 |
140 | 140 | 140 | 160 | 160 190 * |
160 190 * |
160 165 190 * |
160 * |
| Maximum operational opening dynamic shock at VNE and MTOW | kN/G | 4,3 | 5,5 | 7,8 | 13,1 | 14,5 | 18,5 | 22,5 26,3 26,3 |
25,0 | |
| Tested total time of full canopy in VNE and MTOW | sec. | 0,5-2,5 | 1,5 | 1,7 | 1,7 | 1,3-2,0 | 1,4-2,1 | 1,5-2,3 | 1,5 2,5 |
3,2-3,6 |
| Descending recorded at 1000m/AMSL for MTOW | m/s | 3,6-6,1 | 4,5-6,3 | 6,3 | 6,3 | 6,3 | 6,5 | 6,7 | 6,8 7,1 |
7,3 |
| Minimum projected rescue height for horizontal fly | m./Km/h | 5/0 50/0 |
30/60 | 35/60 | 35/60 | 40/60 | 40/65 | 40/65 | 40/65 | 80/60 |
| Method ejection | Ballistic device | hand deployed / ejection rocket* | hand deployed / ejection rocket | hand deployed /ejection rocket | hand deployed /Container rocket | Container sleeve-rocket | Container sleeve-rocket | Container sleeve-rocket | Container | |
Canopy |
||||||||||
| Area | m2 | 1,1-16 | 28 | 32 | 36 | 43 | 60 | 70 | 92 | 100 |
| Number of lines and panels | 7-14 | 14 | 14 | 16 | 18 | 24 | 24 | 24 | 24 | |
| Nominal diameter | m | 1,1-4,1 | 5,4 | 5,8 | 6,0 | 6,2 | 7,2 | 8,3 | 9,2 | 10,6 |
| The central cord | Yes/No* | Yes | Yes | Yes | No | Yes | Yes | Yes | Yes | |
| Ballistic device | Rocket engine 120 | Rocket engine MK4 | ||||||||
| Igniter – mechanical ignition | Activator | Dual primer | Dual primer | |||||||
| Way of activation | mechanical / electrical | mechanical / electrical | mechanical / electrical | mechanical / electrical | mechanical / electrical | mechanical / electrical | mechanical / electrical | |||
| Stationary rocket engine pull | – | 480 N/sec. 49 Kg | 670 N/sec. 68 Kg | |||||||
| Maximum rocket engine pull | – | 750 N/sec. 76 Kg | 930 N/sec. 94 Kg | |||||||
| Ballistic and drawing device weight | – | 2,0 Kg | 2,62 Kg | |||||||
| Burn time (- 40°C – +60°C) | 1 sec. ± 0,2 sec. | |||||||||
| Cycle Exchange 6 years | lifetime 30 years | |||||||||
| Dimensions | ||||||||||
| Soft pack B1-LxWxD B2-LxWxD |
cm cm |
ø10 x 7-19 | 28x23x10 | 28x23x11 | 28x23x11 | 11x20x37,5 | 15x25x40 | 15x25x45 | 15x25x52 | – – |
| Dimensions B1-B13 in products | mm | – | individual | individual | individual | – | B1-B11 | B1-B11 | B1-B11 | – |
| OUT/INr | length diameter |
– – |
– – |
– – |
– – |
– – |
480 185 |
580 185 |
630 185 |
680 185 |
| IN/OUT # / Soft R + (0,75kg) |
Kg | – | – | – | – | 10,9 # | 11,3 # | 12,3 # | 13,6 # | |
| Total weight GRS Soft/modifications rocket ♦ |
Kg | – 0,45-0,7 |
2,1 4,1 ♦ |
2,3 4,3 ♦ |
2,5 4,5 ♦ |
5,9 ♦ | 8,5 ♦ | 9,2 ♦ | 10,8 ♦ | 13,6 # |
Note: GBS 10 Multicopter is only a summary of all the products for the drones and UAV Multicoptery.
Note 2:* => Slider
Note 3: GP-2S, GP-3S, GP-36S a GP-40S are hand deployed chutes
Запасни парашути за Class 120 Kg Ultralights Gliders Gyro- Helicopters S-LSA
For videos and detailed information click on the product name.
| TYPES | GRS 4/6 225 40m2 | GRS 4 240 40m2 | GRS 4 260 40m2 | GRS 4 270 60m2 | GRS 4 350 70m2 | GRS 5 472 96m2 | GRS 5 560 115m2 GYRO |
GRS 5 560 115m2 | |
|---|---|---|---|---|---|---|---|---|---|
| tested by Total safety coefficient of the canopy by ASTM F2316-12 |
Test ASTM 1,5 | Test DULV R31-11 | Test DULV R35-13 | Test ASTM 1,5 | Test ASTM 1,5 | Test DULV R21/01-1 Test DULV R21/01-11 |
Test LAA ČR | Test ASTM 1,5 | |
| Allowed max. operational weight (MTOW) | Kg | 110 225 |
240 | 260 | 270 | 350 | 472,5 450 |
560 | 560 |
| Allowed never exceed speed for use (VNE) | Km/h | 350 260 |
240 | 200 | 230 | 220 | 251 260 |
225 | 250 |
| Maximum operational opening dynamic shock at VNE and MTOW | kN/G | 11,5 12,3 |
13,1 | 13,1 | 14,5 | 18,5 | 22,5 | 24,0 | 26,0 |
| Tested total time of full canopy in VNE and MTOW | sec. | 3,0-3,5 | 3,0 | 3,5 | 2,5-3,0 | 2,5-3,0 | 3,0-3,4 | 3,0-4,0 | 3,5-4,3 |
| Descending recorded at 1000m/AMSL for MTOW | m/s | 6,9-7,2 | 6,9 | 7,2 | 6,6 | 6,6 | 6,7 | 6,8 | 6,8 |
| Maximum load-LIMIT Max. speed |
Kg Km/h |
260 200 |
260 200 |
260 200 |
280 205 |
360 205 |
535 190 |
570 190 |
560 250 |
| Maximum operation dynamic impact | kN | 13,1 | 13,1 | 13,1 | 14,5 | 18,5 | 25,5 | 26,0 | 26,0 |
| Minimum projected rescue height for horizontal fly | m./Km/h | 70/45 | 70/45 | 70/45 | 70/65 | 70/65 | 60/45 | 70/45 | 80/65 |
| Method ejection | Container Short sleeve | Container Short sleeve | Container Short sleeve | Container Short sleeve | Container Short sleeve | Container Short sleeve | Container Short sleeve | Container Short sleeve | |
Canopy |
|||||||||
| Area | m2 | 43 | 43 | 43 | 60 | 70 | 96 | 115 | 115 |
| Number of lines and panels | 18 | 18 | 18 | 24 | 24 | 24 | 26 | 26 | |
| Nominal diameter | m | 5,9 | 5,9 | 5,9 | 7,2 | 8,3 | 9,6 | 10,4 | 10,4 |
| Quantity of slots/Slider* | Yes | Yes | Yes | Yes * | Yes * | Yes * | Yes * | Yes * | |
| Ballistic device | Rocket engine 120 | Rocket engine MK4 | |||||||
| Igniter – mechanical ignition | Dual primer | Dual primer | |||||||
| Stationary rocket engine pull | 480 N/sec. 49 Kg | 670 N/sec. 68 Kg | |||||||
| Maximum rocket engine pull | 750 N/sec. 76 Kg | 930 N/sec. 94 Kg | |||||||
| Ballistic and drawing device weight | 2,0 Kg | 2,62 Kg | |||||||
| Burn time (- 40°C – +60°C) | 1 sec. ± 0,2 sec. | ||||||||
| Cycle Exchange 6 years | lifetime 30 years | ||||||||
| Dimensions | |||||||||
| Soft pack B1-LxWxD B2-LxWxD |
cm cm |
11x20x37,5 – |
11x20x37,5 – |
11x20x37,5 – |
15x25x40 16x27x32 |
15x25x46 16x27x37 |
15x25x52 16x27x42 |
16,5x25x54 19x25x49 |
16,5x25x54 19x25x49 |
| Dimensions B1-B13 in products | mm | B1-B12 | B1-B12 | B1-B12 | B1-B12 | B1-B12 | B1-B12 | B1-B13 | B1-B13 |
| OUT/INr | length diameter |
– – |
– – |
– – |
480 185 |
580 185 |
630 185 |
– – |
– – |
| Weight unit – GRS | Kg | 5,3 | 5,3 | 5,3 | 8,2 9,6 # |
8,9 12,6 |
10,1 12,6 # |
13,3 | 13,3 |
| Drawing sling length weight |
m. Kg |
4,5 0,6 |
4,5 0,6 |
4,5 0,6 |
4,5 0,6 |
5,0 0,67 |
5,0 0,67 |
5,5 0,74 |
6,0 0,8 |
| IN/OUT # / Soft R + (0,75kg) |
Kg | – | – | – | 10,2 # | 11,1 # | 13,3 # | – | – |
| Total weight±4% GRS Soft B GRS Soft B2 |
Kg | 5,9 | 5,9 | 5,9 | 8,8 | 9,6 | 10,9 | 12,6 | 12,6 |
Запасни парашути за Ultralights UAV Gliders Experimentals VLA S-LSA Amfibie
GRS запасни парашути – new series 6/2012 / Patent No.: US,997,535 B2 of Aug.16,2011
For videos and detailed information click on the product name.
TYPES |
GRS 6 90-120 SD 25m2 UAV |
GRS 6 375 SD 70m2 |
GRS 6 375 SD Speedy/H 70m2 |
GRS 6 473 SD Napkin 85m2 |
GRS 6 473 SD Napkin/H 85m2 |
GRS 6 473 SD Speedy 96m2 DULV |
GRS 6 473 SD Speedy 96m2 |
GRS 6 473 SD Speedy H/FF 96m2 |
GRS 6 600 SD Speedy 115m2 |
GRS 6 600 SD Speedy 115m2 DULV |
GRS 6 600 SD Speedy FF 115m2 |
|---|---|---|---|---|---|---|---|---|---|---|---|
Total safety coefficient of the canopy by ASTM F2316-12 |
Test ASTM 1,5 | Test ASTM 1,5 | Test ASTM 1,5 | Test ASTM 1,5 | Test ASTM 1,5 | Test DULV R29-07 | Test ASTM 1,5 | Test ASTM 1,5 | Test ASTM 1,5 | DULV R10/18-2 | Test ASTM 1,5 |
Allowed max. operational weight (MTOW) Kg |
90 90-120 90 |
375 415 |
375 375 |
473 500 |
473 500 473 |
473 525 |
473 525 |
473 525 473 |
600 650 |
600 | 600 650 600 |
Allowed never exceed speed for use (VNE) Km/h |
410 290 250 |
325 290 |
350 400 |
325 290 |
350 300 390 |
310 290 |
325 300 |
350 320 400 |
315 280 |
335 | 350 320 400 |
Maximum operational opening dynamic shock at VNE and MTOW kN/G |
11,0 12,4-15,6 15,6 |
21,0 24,4 |
21,4 23,0 |
23,8 27,3 |
23,8 27,3 25,0 |
23,6 27,5 |
23,6 27,5 |
23,6 28,8 26,0 |
26,7 26,4 |
26,7 | 26,9 26,7 28,0 |
Tested total time of full canopy in VNE and MTOW sec. |
3,3 2,1 1,2 |
4,3 | 4,8-5,5 | 5,0 | 5,9-6,4 | 4,6 | 4,6 | 5,8-6,3 | 5,6 | 6,0 | 6,0-6,5 |
Overall time of full canopy stretching at the speed of 95 km/h. and at the allowed load sec. / km/h |
3,3/180 3,2/120 3,0 |
4,3 | 4,8-5,5 | 4,7 | 5,1-5,3 | 4,3 | 4,3 | 4,5-5,0 | 5,2 | 6,0/65 | 5,6-5,8 |
Descending recorded at 1000m/AMSLMin. Max MTOW m/sDescending recorded at 1500m/AMSL m/s |
6,0-6,9 – |
7,1-7,5 | 7,1-7,5 | 7,5-7,7 | 7,5-7,7 | 7,1-7,5 | 7,1-7,5 | 7,1-7,5 | 7,1-7,3 7,3-7,5 |
7,5 – |
7,1-7,3 7,3-7,5 |
Maximum load at speed 250 km/h – Kg |
473 | 473 | 550 | 550 | 578 | 578 | 578 | 750 | 750 | 750 | |
Maximum operational opening dynamic shock at the speed 250 Km/h – kN |
24,0 | 23,9 | 31,1 | 31,1 | 34,0 | 34,0 | 34,0 | 32,1 | 32,1 | 32,0 | |
Minimum projected rescue height for horizontal fly m./km/h |
80/80 | 100/80 160/≥300 | 110/90 | 120/90 160/≥300 | 80/90 | 80/90 | 100/90 160/≥300 | 110/90 | 110/90 | 120/90 160/≥300 | |
Method ejection |
Container Short sleeve | Container Short sleeve | Container Short sleeve | Short sleeve | Short sleeve | Container Short sleeve | Container Short sleeve | Container Short sleeve | Container Short sleeve | Container Short sleeve | Container Short sleeve |
Canopy |
|||||||||||
Area m2 |
25 | 70 | 70 | 85 | 85 | 96 | 96 | 96 | 115 | 115 | 115 |
Number of lines and panels |
18 | 24 | 24 | 24 | 24 | 24 | 24 | 24 | 26 | 26 | 26 |
Nominal diameter m |
5,1 | 8,3 | 8,3 | 9,2 | 9,2 | 9,6 | 9,6 | 9,6 | 10,6 | 10,6 | 10,6 |
Quantity of slots/Slider |
3 | 18 | 24/36 | 18 | 24/36 | 18 | 18 | 24/36 | 22 | 26 | 34/39 |
Ballistic device |
Rocket engine 120 | Rocket engine MK4 | |||||||||
Igniter – mechanical ignition |
Dual primer | Dual primer | |||||||||
Stationary rocket engine pull |
480 N/sec. 49 Kg | 670 N/sec. 68 Kg | |||||||||
Maximum rocket engine pull |
750 N/sec. 76 Kg | 930 N/sec. 94 Kg | |||||||||
Ballistic and drawing device weight |
2,0 Kg | 2,62 Kg | |||||||||
Burn time (- 40°C – +60°C) |
1 sec. ± 0,2 sec. | 1 sec. ± 0,2 sec. | |||||||||
Cycle Exchange 6 years |
lifetime 30 years | ||||||||||
Dimensions |
|||||||||||
Soft packB1-LxWxD cmB2-LxWxD cm |
As required | 44x25x15 37x27x16 |
44x25x15 37x27x16 |
– – |
– – |
50x25x15 42x27x16 |
50x25x15 42x27x16 |
50x25x15 42x27x16 |
54x25x16,5 49x25x19 |
54x25x16,5 49x25x19 |
44x28x23 36x38x20 |
Dimensions B1-B13 in products mm |
B1-B13 | B1-B13 | B1-B13 | B1-B13 | B1-B13 | B1-B13 | B1-B13 | B1-B14 | B1-B14 | B1-B13 | |
OUT/INrmmø |
560 185 |
560 185 |
560 185 |
560 185 |
630 185 |
630 185 |
630 185 |
– – |
– – |
– – |
|
Weight unit – GRS Kg |
3,4 | 8,6 10,7 # |
8,6 10,7 # |
9,1 11,2 # |
9,1 11,2 # |
10,1 12,6 |
10,1 12,6 |
10,1 12,6 # |
11,5 | 11,5 | 11,5 |
Drawing slinglength m.weight Kg |
4,0 0,4 |
4,5 0,6 |
4,5 0,6 |
4,5 0,6 |
4,5 0,6 |
5,0 0,67 |
5,0 0,67 |
5,0 0,67 |
5,5 0,74 |
5,5 0,74 |
5,5 0,74 |
IN/OUT #/ Soft R + (0,75kg) Kg |
11,3 # | 11,3 # | 11,8 # | 11,8 # | 13,1 # | 13,1 # | 13,1 # | – | – | – | |
Total weight±4% KgGRS Soft BGRS Soft B2 |
5,8 (including rocket) | 9,2 | 9,2 | 9,5-9,8 | 9,5-9,8 | 10,8 | 10,8 | 10,9 | 12,3 | 12,3 | 12,3 |
Note*: Запасни парашути GRS 6/375 Speedy/H, GRS 6/473 Napkin Speedy /H, GRS 6/473 Speedy/H and GRS 6/600 SD Speedy FF/H it also produces up to speed TAS 370-400 km/h.!
Запасни парашути за Amfibie UAV Experimental Four–Seater Plane
GRS – new series 6/2012 / Patent No.: US,997,535 B2 of Aug.16,2011
For videos and detailed information click on the product name.
| TYPES | GRS 6 650-700 SD Speedy 140m2 |
GRS 6 650-700 SD/FF Speedy 140m2 |
GRS 6 750 SDS/FF 140m2 |
GRS 6 800-990 SDS 175m2 |
GRS 6 990-1190 SDS/FF 245m2 |
GRS 6 1200-1390 SDS/FF 245m2 |
GRS 6 1200-1320 SDS/FF 245m2 |
GRS 6 1420-1640 SDS/FF 245 m2 |
|
|---|---|---|---|---|---|---|---|---|---|
Total safety coefficient of the canopy by ASTM F2316-12 |
Test ASTM 1,5 | Test ASTM 1,5 | Test ASTM 1,5 | Test ASTM 1,5 | Test ASTM 1,5 | Test ASTM 1,5 | Test ASTM 1,5 | Test ASTM 1,5 | |
Allowed max. operational weight (MTOW) |
Kg | 650 700 750 |
650 700 |
750 700 |
800 950 990 |
990 1190 |
1200 1390 |
1200 1320 |
1420 1640 |
Allowed never exceed speed for use (VNE) |
Km/h | 325 295 250 |
350 325 |
300 325 |
385 373 340 |
365 350 |
350 260 |
380 380 |
320 250 |
Maximum operational opening dynamic shock at VNE and MTOW |
kN/G | 25,2/3,9 27,2/3,9 28,8 |
25,2/3,9 26,6/3,9 |
28,8/3,9 27,5/3,9 |
39,8/5,0 40,3/4,5 41,6/4,2 |
39,2/4,0 42,1/3,5 |
54,8/4,7 62,0/4,8 |
54,8/4,7 62,0/4,8 |
59,0/4,2 62,2/3,9 |
Tested total time of full canopy in VNE and MTOW |
sec. | 5,6 | 6,0 | 6,0 6,2 |
5,7 | 5,8 | 5,9 | 6,0 | 6,0 |
Overall time of full canopy stretching at the speed of 95 km/hod. and at the allowed load |
sec. | 6,0 | 6,2 | 6,0 6,2 |
6,0 | 6,4 | 6,5 | 6,0 | 6,0 |
Descending recorded at 1000m/AMSLMin. Max MTOW m/sDescending recorded at 1500m/AMSL |
m/s | 6,7-7,2 6,9-7,4 |
6,7-6,9 6,9-7,2 |
7,2-6,9 7,4-7,2 |
5,7-6,4 5,8-6,9 |
5,4-5,9 5,6-6,1 |
5,6-6,1 6,0-6,5 |
5,9-6,3 6,1-6,5 |
6,5-7,0 6,7-7,2 |
Maximum load at speed 250 km/h |
Kg | 793 | 793 | 793 | 1170 | 1438 | 1500 | 1645 | 1645 |
Maximum operational opening dynamic shock at the speed 250 Km/h |
kN | 32,3 | 32,3 | 32,3 | 44,9 | 47,5 | 57,8 | 63,0 | 63,0 |
Minimum projected rescue height for horizontal fly |
m. | 120 | 140 | 140 | 140 | 150 | 150 | 150 | 150 |
Method ejection |
Container | Container | Container | Short sleeve | Short sleeve | Short sleeve | Short sleeve | Short sleeve | |
Canopy |
|||||||||
| Area | m2 | 140 | 140 | 140 | 175 | 245 | 245 | 245 | 245 |
| Number of lines and panels | 28 | 28 | 28 | 40 | 40 | 40 | 56 | 56 | |
| Nominal diameter | m | 11,23 | 11,23 | 11,23 | 13,1 | 15,6 | 15,6 | 15,6 | 15,6 |
| Quantity of slots/Slider* | 24 | 42 | 42 | 160* | 160* | 160* | 224* | 224* | |
| Ballistic device | Rocket engine MK4 | Rocket engine 222 | |||||||
| Igniter – mechanical ignition | Dual primer | Dual primer | |||||||
| Stationary rocket engine pull | 670 N/sec. 68 Kg | 1000 N/sec. 102 Kg | |||||||
| Maximum rocket engine pull | 930 N/sec. 94 Kg | 1370 N/sec. 139 Kg | |||||||
| Ballistic and drawing device weight | 2,62 Kg | 2,91 Kg | |||||||
| Burn time (- 40°C – +60°C) | 1 sec. ± 0,2 sec. | ||||||||
| Cycle Exchange 6 years | lifetime 30 years | ||||||||
| Dimensions | |||||||||
| Soft pack B1-LxWxD B2-LxWxD |
cm cm |
B1-B13 – |
B1-B13 – |
B1-B13 – |
48x34x23 48x38x21 |
64x34x23 63x38x21 |
64x34x23 63x38x21 |
67,5x38x23 72x38x21 |
67,5x38x23 72x38x21 |
| Weight unit – GRS | |||||||||
| Drawing sling length weight |
m. Kg |
2x 6 0,8 |
2x 6 0,8 |
2x 6 0,8 |
3x 4 0,9 |
3x 5 1,1 |
3x 6 1,2 |
4x 8 1,7 |
4x 8 1,7 |
| Total weight±4% GRS Soft B GRS Soft B2 |
Kg | 14,1 – |
14,1 – |
14,8 – |
– 21,7 |
– 27,5 |
– 27,5 |
– 31,5 |
– 31,5 |
Запасни парашути GRS