Rescue systems GRS 5

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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.

Backorder:Usually 10-20 days

SKU GRS5

Brand GRS Galaxy rescue systems

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 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 DULV R21/01-1 Test DULV R21/01-11	Test LAA ČR	Test ASTM 1,5
Allowed max. operational weight (MTOW)	Kg	472,5 450	560	560
Allowed never exceed speed TAS for use (VNE)	Km/h	251 260	225	250
Maximum operational opening dynamic shock at VNE and MTOW	kN/G	22,5	24,0	26,0
Tested total time of full canopy in VNE and MTOW	sec.	3,0-3,4	3,0-4,0	3,5-4,3
Descending recorded at 1000m/AMSL for MTOW	m/s	6,7	6,8	6,8
Maximum load-LIMIT Max. speed	Kg Km/h	535 190	570 190	560 250
Maximum operation dynamic impact	kN	25,5	26,0	26,0
Minimum projected rescue height for horizontal fly	m./Km/h	60/45	70/45	80/65
Method ejection		Container Short sleeve	Container Short sleeve	Container Short sleeve
Area	m²	96	115	115
Number of lines and panels		24	26	26
Nominal diameter	m	9,6	10,4	10,4
Quantity ofslots/Slider*		Yes *	Yes *	Yes *
Ballistic device
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
Soft pack B1-LxWxD B2-LxWxD	cm cm	15x25x52 16x27x42	16,5x25x54 19x25x49	16,5x25x54 19x25x49
Dimensions B1-B13 in products	mm	B1-B12	B1-B13	B1-B13
OUT/INr	length diameter	630 185	--- ---	--- ---
Weight unit - GRS	Kg	10,1 12,6 #	13,3	13,3
Drawing sling length weight	m. Kg	5,0 0,67	5,5 0,74	6,0 0,8
IN/OUT # / Soft R + (0,75kg)	Kg	13,3 #	---	---
Total weight±4% GRS Soft B GRS Soft B2	Kg	10,9	12,6	12,6

Documents

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

Video

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