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Rescue systems GRS 3

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aucun

The GRS system is designed for quick deployment to enable the rescue of crew and aircraft from the lowest possible height. In other systems the parachute is gradually pulled out from the top, exposing the length of the material to distortion by air currents and damage by contact with airframe or detached parts thereof. The GRS canopy is kept contained in a harness until the suspension ropes are fully extended at 15-18m above the airplane (depending on model), where it is then extracted for safe inflation. This design minimises the danger of damage to the fabric and suspension ropes during deployment. Inflation of the canopy starts in 0,4 to 0,7 seconds from activation of the system. The system is designed with reserve capacity to work even under extreme conditions.

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Backorder:Usually 10-20 days
SKU GRS3
Description

Galaxy offers you a state of the art rescue system.

The system is designed for the rescue of crew and aircraft, specifically for 1 and 2-seat light aircraft, ultralights and experimental aircraft and lately for General Aviation aircraft and unmanned aircraft. The product is certificated by LAA ČR, USA, Australia,Canada,South Africa and the DULV, BAM Germany and complies with the conditions for purchase of rocket systems in the trade net of ČR, USA and EC. The system has earned the patent certificate PV 1859-94.

Technical data
TYPES   GRS 3 GRS 3 270 60m2 GRS 3 350 70m2 GRS 3 450 922 GRS 3
180 450 100
GP-40S m2 GYRO
40m2  
tested by:   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
Total safety coefficient of the canopy by ASTM F2316-12
Allowed max. operational weight (MTOW) Kg 180-190 270 350 475 560
270 350 475
Allowed never exceed speed TAS for use (VNE) Km/h 160 160 160 160 160 *
190 * 190 * 190 *
Maximum operational opening dynamic shock at VNE and MTOW kN/G 13,1 14,5 18,5 22,5 25
Tested total time of full canopy in VNE and MTOW sec. 1,3-2,0 1,4-2,1 1,5-2,3 1,8-2,5 3,2-3,6
Descending recorded at 1000m/AMSL for MTOW m/s 6,3 6,5 6,7 6,8 7,3
Minimum projected rescue height for horizontal fly m./Km/h 40/60 40/65 40/65 40/65 80/60
             
Canopy
Area m2 43 60 70 92 100
Number of lines and panels   18 24 24 24 24
Nominal diameter m 6,2 7,2 8,3 9,2 10,6
The central cord   No Yes Yes Yes Yes
Ballistic device     Rocket engine MK4
Igniter – mechanical ignition     Dual primer
Stationary rocket engine pull     670 N/sec. 68 Kg
Maximum rocket engine pull     930 N/sec. 94 Kg
Ballistic and drawing device weight     2,62 Kg
Burn time (- 40°C - +60°C)    
Cycle Exchange 6 years    
Dimensions
Soft pack cm 11x20x37,5 15x25x40 15x25x45 15x25x52 ---
B1-LxWxD cm ---
B2-LxWxD    
Dimensions B1-B13 in products mm --- B1-B11 B1-B11 B1-B11 ---
OUT/INr length --- 480 580 630 680
diameter --- 185 185 185 185
IN/OUT # Kg --- 10,9 # 11,3 # 13,3 # 13,6 #
/ Soft R + (0,75kg)
Total weight Kg 5,9 ♦ 8,5 ♦ 9,2 ♦ 10,8 ♦ 13,6 #
GRS Soft/modifications rocket ♦
Method ejection   throwing Container rocket Container sleeve-rocket Container sleeve-rocket Container sleeve-rocket Container
Documents

https://www.galaxysky.cz/manual/en_uni.pdf

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