GRS – Galaxy Rescue Systems – Technical data
On the basis of this technical information, you can find out which rescue system is suitable for your aircraft.
Additional information about each of the spare parachutes can be found in our online store.
Galaxy Rescue Systems for DRON MULTICOPTER UAV
For videos and detailed information click on the product name.
TYPES |
GBS 10/30 DRON MULTICOPTER UAV |
GBS 10/50 DRON MULTICOPTER UAV |
GBS 10/150 DRON MULTICOPTER UAV |
GBS 10/350 DRON MULTICOPTER UAV |
GBS 10/350 Speedy MULTICOPTER DRON UAV |
GBS 10/650 DRON MULTICOPTER UAV |
GBS 10/650 Speedy MULTICOPTER DRON UAV |
||
---|---|---|---|---|---|---|---|---|---|
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 BrnoVZLÚ Praha |
Yes Yes |
Yes Yes |
Yes Yes |
Yes Yes |
Yes Yes |
Yes Yes |
Yes Yes |
|
Canopy |
|||||||||
Number of linespandanels |
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 |
Galaxy Rescue Systems for 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 byTotal 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 packB1-LxWxDB2-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 weightGRS 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

Galaxy Rescue Systems for 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 byTotal 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 |
Maximumoperational 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-LIMITMax. speed |
Kg Km/h |
260 200 |
260 200 |
260 200 |
280 205 |
360 205 |
535 190 |
570 190 |
560 250 |
Maximum operationdynamic 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 packB1-LxWxDB2-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 slinglengthweight |
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 BGRS Soft B2 |
Kg | 5,9 | 5,9 | 5,9 | 8,8 | 9,6 | 10,9 | 12,6 | 12,6 |

Galaxy Rescue Systems for Ultralights UAV Gliders Experimentals VLA S-LSA Amfibie
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 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 |
Numberof 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/INr mm
|
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*: 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.!

Galaxy Rescue Systems for 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 packB1-LxWxDB2-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 |
