Technical data

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 TAS 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

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 TAS 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

tab1.jpg

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 TAS 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

tab2.jpg

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 TAS 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/AMSL
Min. Max MTOW m/s
Descending 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 pack
B1-LxWxD cm
B2-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
ø

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 sling
length 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% Kg
GRS Soft B
GRS 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.!

tab3.jpg

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 TAS 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/AMSL
Min. Max MTOW m/s
Descending 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

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