Specifications. Specifications Parts of the parachute system

2.2. LAYING THE PARACHUTE SYSTEM D-10

Laying parachute system D-10 is produced in six stages.

First stage. Checking the presence and serviceability of parts of the main

parachute, preparing them for packing

Elements of the 1st stage

1. Pull out the parachute system to its full length. The reserve parachute (if it is not required to be repacked) and the parachute bag are placed on the upper edging panel.

2. Check the fastening of the parachute (shelf number), as well as the correspondence of the numbers of the passport and the main dome.

3. Check for availability of parts.

4. Check the technical condition of the parts.

5. Check the installation of the interlock cords at the free ends.

6. Install the manual release link cable into the flexible hose and insert the ring into the pocket.

7. Remove the safety parachute device from the backpack, inspect it externally and put it on the upper edging panel.

8. Check the position of the lines and that they are not tangled.

9. If necessary, unravel the lines.

The laying sheet is completely spread out (1) (Fig. 2.32) and secured with crutches. The laying sheet is covered with a bed sheet (4), the parachute system is taken out of the bag, placed in the middle of the laying sheet (table) and pulled out to its full length. The detachable parts are laid out in the following order: the stabilizing c-stem (10) is placed to the right of the top of the dome (12) and the main parachute chamber (11); laying accessories (5) - at a distance of 2 m from the bed sheet (4); the manual release link ring is inserted into the pocket on the main strap after inspection suspension system, and the cable is passed into the hose. The parachute bag (6) is folded and, together with the reserve parachute (7) and the AD-3U-D parachute device, are placed on the upper edging panel (2).

First, they check the numbers on the parachute passport and the main canopy. After making sure they match, proceed to check technical condition parachute system. They take the camera of the stabilizing system, make sure that the carabiner (4) is in good condition (Fig. 2.33), whether the tapes attaching the carabiner to the camera and the metal rings (2) are securely sewn, whether the fabric of the camera (1) is not damaged and whether the ties are in good order. After checking, the stabilizing parachute chamber is placed on the upper edging panel next to the reserve parachute. When examining the stabilizing system and the chamber of the main parachute, they check for tears and burns of the fabric, violations of the lines at the points of attachment of reinforcing tapes (3) and lines, damage to pockets, honeycombs (7), removable rubber honeycombs (9), bridles, loops (5), elastic ring (8), aprons (10). The connection unit (6) and the presence of a clip at the point of attachment of the parachute link to the bridle of the camera and the main parachute canopy are checked. In case of detection of a rush of rubber cells, they are removed and replaced with new ones.

Brand, brand "href="/text/category/klejm__klyejm/" rel="bookmark">the manufacturer's stamp was on top. The top of the dome is attached with a bridle to a crutch holding the end of the laying cloth, or to another device. One person takes the main parachute for the slings at the chrome -

https://pandia.ru/text/78/374/images/image007_57.gif" alt="(!LANG:Signature:" align="left" width="212" height="256 src=">При осмотре подвесной системы проверяют ее металлические детали: карабины и их пружины, кольца, пряжки (изогнутые, полукольца и др.), скобы крепления запасного парашюта. На металлических деталях не должно быть коррозии и других повреждений.!}

They check the installation of locking cords (2) of the free ends (1) (Fig. 2.35), the presence of a fastener made of nylon thread on them, the serviceability of the ribbons and lines of the suspension system and the pocket (6) for the ring (5). When using a parachute system using the rolls of the free ends of the harness, the locking cords of the free ends are removed. To do this, carefully cut the bartack of the ends of the cord, untie the knots and remove the blocking cords.

Check fastening of the buckles with toothed bridges (8) to the straps of the dorsal-shoulder girths (7) in the area of the marks (11). Adjusting tapes are attached to the double buckles on the main strap (Fig. 2.37), and tapes for tightening the corners of the satchel are attached to the double rings.

When inspecting the satchel, they check whether the stiffening frame is deformed, whether there are any tears in the fabric of the valves and the bottom of the satchel, whether the pocket and ties are in good order.

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for fastening parachute device whether the ring for locking the loop of the parachute link and the ring for attaching the camera with a stabilizing parachute are securely fixed, whether the rubber honeycomb on the right valve of the backpack is in good order.

They check the serviceability of the hose of the manual opening link and its fastening to the knapsack, the sewing of the regulating tapes and loops for attaching the suspension system to the bottom of the knapsack, the bands for pulling up the corners of the knapsack, and also pay attention to whether the fabric and bands of the knapsack are damaged, check the serviceability of knapsack carabiners and tapes for attaching a spare parachute.

When examining a two-cone lock, they check whether it is securely attached to the knapsack, whether there are dents, nicks, corrosion and dirt on the two-cone lock, whether there are any obstacles to opening and closing the shutter. If dirt and dust are found on the lock, they must be removed with a dry cloth.

Inspecting the manual opening link, make sure that there are no damages and burrs on the wire loop, its braid and soldering are not broken, there are no breaks in the cable threads and the cable stop is securely sealed. After checking, the ring (5) is inserted into the pocket (6) on the main strap of the suspension system, and the cable (4) is threaded into the hose (3) (Fig. 2.35).

When inspecting a parachute bag, they check for fabric rips and damage to the handles, the presence and serviceability of a tightening cord and a metal tag. After making sure that the bag is in good condition, it is carefully folded and placed on the laying panel.

The AD-3U-D-165 parachute device is placed on the upper edging panel next to the reserve parachute (on the folded parachute bag).

If defects are found during the inspection of the parachute system, then its repair or replacement of defective parts must be carried out in a VDT repair shop. After the defects have been eliminated, the laying of the parachute system is permitted only after verification by an officer of the airborne service.

Control elements of the 1st stage

1. Connecting the harness to the backpack:

Buckles with a toothed bridge are connected to the dorsal-shoulder

girths;

The adjustment straps are connected to the main strap buckles.

2. Inserting the manual release link ring into the pocket on the main harness strap and threading the cable through the hose.

3. The presence of locking cords, if the parachute system is used without rolling the free ends. (The absence of locking cords when using a parachute system with a roll of free ends).

4. Correct installation of the pinning device (with the textile fastener unfastened).

5. No tangling of lines.

6. Knot connecting the loop of the parachute link with the bridles of the canopy and the chamber of the main parachute, the presence of a clip on the loop.

7. Serviceability of the parachute device (checked by an instrument technician

and automatic devices).

Stage control position

Styling- dropping to one knee facing the inspector, holding the satchel vertically with his left hand. In the same hand, he holds the cable loop of the manual opening link and the rubber honeycomb of the right valve of the knapsack, with his right hand he presents the ratchet device for verification with the textile fastener unfastened.

Helping- standing at the top of the dome, in right hand holds the knot connecting the bridles of the canopy of the main parachute and its chamber with the loop of the parachute link, presents for verification the bartack on the loop. In the left hand, at the level of the belt, he holds the dome of the stabilizing system by the top.

Second phase. Laying the canopy of the main parachute

and putting a camera on him

Elements of the 2nd stage

1. Put loops of lines No. 13A and 13B on the loop of the sling No. 12, straighten the panel, closing the gap between the slings No. 13A and 13B.

2. Present the position of the lines and the first panel for control.

3. Lay the left half of the dome (up to the factory mark) and fix it with three weights.

4. Throw the right side of the dome onto the stacked left half.

5. Lay the right half of the dome.

6. Eliminate the gap between the right and left halves of the dome.

7. First bend the right side of the edge and the base of the dome, then the left side to the width of the chamber.

Put the camera on the dome. Check that the dome is stacked correctly and that the camera is attached to the dome.

The order of execution of the elements of the stage

Find sling No. 12, marked with a red or orange sleeve at the edge of the dome, and lay it along the center line of the laying panel, the rest of the dome is placed to the right of it. A loop of sling No. 13A is placed on the loop of sling No. 12, the dome panel located between these slings is straightened to the top of the dome. A loop of slings No. 13B is placed on the loop of slings No. 13A, the slings and the dome panel are slightly pulled to close the gap between slings No. 13A and 13B. The position of the dome is fixed with three weights from the set of laying accessories: one weight is placed on the edge of the first panel, the second - at the edge of the rest of the dome, the third - at the top of the gap. They represent the position of the lines No. 12, 13A and 13B and the first panel of the dome for control to the unit commander and the officer of the airborne service, while the laying person stands at the edge of the main dome facing the inspector, helping behind him.

https://pandia.ru/text/78/374/images/image014_10.jpg" align="left" width="352" height="306 src=">.jpg" align="left" width="280 " height="249 src=">If the right and left halves are at a considerable distance from each other, then they are carefully shifted. To do this, holding a bundle of slings at the edge of the dome, pull the dome by the bridle.

https://pandia.ru/text/78/374/images/image020_6.jpg" align="left" width="465 height=345" height="345"> Align the bottom edge. ts of the suspension system and, holding the edge of the dome in the chamber, gently shaking, pull the lines to their full length.
straighten the folds of fabric formed in the middle part of the dome (Fig. 2.42 a). To do this, holding

Elements of control of the 2nd stage

1. The correct laying of the canopy and the position of the lines.

Being at the knapsack, take the slings of the upper free ends in one hand, and slings No. 24, 1A and 1B in the other. Raising and separating them, go to the edge of the dome and check the division of the dome in half into upper and lower parts. Slings No. 1A, 1B and 24 are on top (Fig. 2.43): on the left - No. 24 and 1A, on the right - No. 1B. A bundle of internal additional lines comes out from the middle of the edge of the dome.

2. Control of the position of the chamber of the main parachute:

The reinforcing tape sewn around the perimeter of the chamber base is on the same level with the edge of the stacked dome;

Honeycombs are on top;

The elastic ring of the lower base of the chamber is located inside the chamber at a distance of 150 - 200 mm from the edge of the dome;

The curve-to-top portion of the dome and the stabilizing system are located to the right of the bottom of the dome;

The canopy extends into the neck of the top of the main parachute chamber, rather than being passed between the chamber bridle bands.

Control position

Styling- kneeling down on one knee at the edge of the dome facing the inspector, holding all the slings with his hand.

Helping- kneeling down at the knapsack facing the inspector, with one hand raises the knapsack, on the forearm of the second hand holds the upper free ends (Nos. 1 and 4) and control lines (Fig. 2.44).

Purpose, device and interaction of parts

The landing parachute system D-10 is designed for training and combat jumps from the An-22, Il-76, An-26 military transport aircraft, from the An-2 aircraft and Mi-6 and Mi-8 helicopters, performed by individual paratroopers or groups of paratroopers of all specialties with full service weapons and equipment or without it, with a total flight weight of a paratrooper of 140 kg.

Technical and operational characteristics

Operating restrictions:
weight of a paratrooper with parachutes, kg	140 – 150
aircraft flight speed, km/h	140 – 400
maximum safe parachute opening height, m
minimum safe application height, m
Stabilization time, s	3 or more
Speed of descent on a stabilizing parachute, m/s	30 – 40
The force required to open a two-cone lock using a manual opening link, kgf, no more
Speed of descent on the main parachute, m/s
Turnaround time in any direction by 180 0 when the lock cord is removed and the free ends of the harness are pulled over, s	no more than 60
Time to turn in any direction by 180 0 with locked free ends of the suspension system, s	no more
Average horizontal forward and backward speed, m/s	not less than 2.6
Height of a paratrooper-paratrooper, m	1,5 – 1,9
Weight of parachute system without parachute bag and parachute device AD-3U-D-165, kg, no more	11,7
Number of uses:
with a total flight weight of a paratrooper-paratrooper of 140 kg, times
including with a total flight weight of a parachutist 150 kg
Shelf life without repacking, months, no more
Warranty period, years
It is allowed to increase the service life, years	up to 20

The D-10 parachute system allows the use of reserve parachutes of the Z-4, Z-5, Z-2 types. Parachute devices AD-3U-D-165, PPK-U-165A-D are used as a safety device for opening a two-cone lock. Parts of the parachute system are inseparable, which excludes their disconnection during the entire landing process.

Parts of the parachute system

1. Camera of the stabilizing system.

2. Stabilizing system (stabilizing strapless parachute).

3. Main parachute chamber.

4. Main parachute (dome with lines).

5. Suspension system.

7. Double cone lock.

8. Manual opening link.

9. Safety parachute device type PPK-U or AD-ZU-D.

10. Parachute bag.

11. Passport.

12. Auxiliary parts and details.

Camera Stabilization System(fig. 1.20) is intended for laying in it the stabilizing dome with slings and the upper part of the stabilizer, as well as for the orderly commissioning of the stabilizing system.

The shape is cylindrical. Material - kapron advice. It consists of a base (4) and those on it: in the upper part - a carabiner (1) for attaching to a cable or extension in an airplane, a lashing tape (7) for tying in a rubber honeycomb, a fuse (6) , drawstring cord (3) for tightening the camera; at the bottom - metal rings (5) for locking with stabilizer rings.

Stabilizing system (stabilizing strapless parachute) It is designed to put into operation a safety parachute device, to ensure a stabilized descent of the parachutist and to open the main parachute.

Stabilizing system ( rice. 1.21 ) consists of a canopy with lines and a stabilizer with a parachute link.

In the pole part of the dome, there is an exhaust device (2) sewn in, which is designed to ensure the filling of the dome and consists of eight pockets. Reinforcing tapes are sewn on the outer side of the dome: radial (3) - from the tape LTKP-15-185 and circular (4) from the tape LTKP-13-70. The edge of the dome is reinforced by folding the fabric to the outer side and stitched onto it on both sides with an LTKP-15-185 tape. Along the lower edge of the dome under the radial reinforcing tapes, the ends of 16 slings made of the ShKP-200 cord are threaded and attached in a zigzag stitch. The length of the outer lines (6) in the free state from the lower edge of the canopy to the stabilizer feather is 0.52 m, and the middle lines (5) are 0.5 m. The canopy has a factory stamp (18): parachute index and year of manufacture.

The stabilizer serves to prevent rotation of the stabilizing parachute and consists of two feathers (7), each of which is made of gray nylon fabric and has the shape of an isosceles triangle. The feathers are stitched in height to form four stabilizer feathers. On the sides of each feather, LTKrP-26-600 ribbons are sewn, forming loops in the upper part, to which lines are attached, and in the lower part passing into a parachute link. A ribbon with a ring (17) is sewn on each side of the feather. The rings serve for locking them with the rings sewn on the chamber of the stabilizing parachute.

The parachute link (8) serves to connect the stabilizing parachute to the satchel during the stabilization stage and to the main canopy at all other stages of work, as well as to remove the stabilizing parachute from the paratrooper and ensure its stable operation. At a distance of 0.45 m from the stabilizer feathers, a loop (9) from the LTKrP-26-600 tape is sewn onto the link, which is intended for attaching the cord for turning on the parachute device. Bottom part the link branches out, forming power tapes (10), at the ends of which buckles (11) of a two-cone lock are sewn. Jumpers made of LTK-44-1600 tape are sewn on both sides of the power tapes. A loop (13) of LTKMkrP-27-1200 tape is sewn between the jumpers, which is designed to attach the stabilizing system to the bridle of the main parachute canopy and to the bridle of its chamber. On the loop there is a check-in tape (12) made of LTKrP-26-600 red nylon tape in three additions and designed for check-in of a removable honeycomb located on the ring of the right valve of the knapsack. One of the lashing concentrators has a loop for attaching to the loop of the parachute link of the stabilizing parachute, the other has a mark limiting the lashing.

The triangle formed from the ribbons is closed on both sides with kerchiefs (14) made of nylon advisor. A guide ring (16) is sewn onto the power tapes between the scarves using tape (15) LTKrP-26-600, through which the parachute device activation cord is passed. On the power tapes near the buckles, arrows are applied with black harmless paint to control the correct installation and installation of power tapes on a two-cone lock.

Parachute stabilizing strapless(Fig. 1.22) consists of a dome, a stabilizer and a parachute link.

The dome (1) has a hemispherical shape with an area of 1.5 m 2 and is made of nylon fabric. Radial reinforcing tapes (3)LTKP-15-185 and circular tapes (2)LTKP-13-70 are stitched on the outer side of the dome. The edge of the dome is reinforced with LTKP-15-185 tape stitched onto it on both sides. The canopy is marked with a factory stamp: parachute index and year of manufacture. _____________________________

The stabilizer serves to prevent rotation of the stabilizing parachute and consists of four feathers (4), which are made of gray nylon fabric. On the surface of each stabilizer feather, on both sides, a reinforcing frame made of LTKP-13-70 tape is sewn. The upper side of each feather is attached to the dome with the help of the bifurcated ends of the reinforcing frame tapes. On the sides of each feather, LTKrP-26-600 ribbons are sewn, which form a parachute link in the lower part. A ribbon with a ring (15) is sewn on each side of the feather. The rings serve for locking them with the rings sewn on the chamber of the stabilizing parachute.

The parachute link (5) is used to connect the stabilizing parachute to the backpack during the stabilization stage and to the main canopy at all other stages of operation, as well as to remove the stabilizing parachute from the main parachute and ensure its stable operation. At a distance of 0.45 m from the stabilizer feathers, a loop (6) from the LTKrP-26-600 tape is sewn onto the link, which is intended for attaching the cord for turning on the parachute device. The lower part of the link branches out, forming power tapes (7), at the ends of which buckles (8) of a two-cone lock are sewn. Jumpers made of LTK-44-1600 tape are sewn on both sides of the power tapes. A loop (10) of LTKMkrP-27-1200 tape is sewn between the jumpers, which is intended for attaching a stabilizing parachute to the bridle of the main parachute canopy and to the bridle of its chamber. On the loop there is a lashing tape (9) made of LTKrP-26-600 nylon tape of red color in three additions and designed for buckling a removable honeycomb located on the ring of the right valve of the knapsack. On one end of the lashing there is a loop for attaching to the loop of the parachute link of the stabilizing parachute, on the other there is a mark limiting the lashing.

The triangle formed from the ribbons is closed on both sides with kerchiefs (11) made of nylon advisor. A guide ring (13) is sewn onto the power tapes between the scarves using tape (12) LTKrP-26-600, through which the parachute device activation cord is passed. On the power tapes near the buckles, arrows are applied with black harmless paint to control the correct installation and installation of power tapes on a two-cone lock.

Main parachute chamber(fig. 1.23) is used for laying the canopy with the lines of the main parachute into it and for its orderly opening. The camera is made of gray nylon fabric and has the shape of a cylinder (when folded).

The surface of the chamber is reinforced with two tapes (2)LTKrP-26-600, which form a bridle in the upper part. For the convenience of laying the dome in the chamber along the upper base of the chamber and the bridle ribbons, our scarf (5). A cord-tie (3) from the ShKP-150 cord, which is designed to tighten the upper base of the chamber, is inserted and attached to the under-bend of the upper base of the camera.

On the base of the camera is sewn:

Nine straight (10) combs with ribbons (11) at the bottom for laying main parachute lines:

Honeycomb spreader (8) with honeycomb rubber (9) from knapsack cord to hold the lines in the comb;

Valve (15) with two pairs of eyelets (14) for passing removable rubber honeycombs (16, 17) and with two pockets (21) for covering bundles of lines; for the convenience of laying the slings, the valve near the eyelets is marked - 1,2,3,4;

Pocket (22) at the top base of the chamber for threading the ends of the cord-tie.

To cover the bundles of slings laid in honeycombs, aprons (7) made of gray nylon fabric with tie ribbons (6) are sewn in the upper part of the chamber.

A ring (20) of an elastic band 29 mm wide is inserted into the hem of the lower part of the chamber, designed to ensure an orderly exit of the main parachute canopy from the chamber.

At the lower base of the chamber, two removable rubber honeycombs are installed and an apron (19) is sewn on, which in turn has two more removable rubber honeycombs.

main parachute(Fig. 1.24) is designed to ensure a safe speed of descent and landing of a parachutist.

Consists of the base of the dome and lines. The base of the dome consists of 24 wedges (1), which form a non-planar circle with an area of 100 m 2 . Each wedge of the dome, in turn, consists of seven wedges, six of which are made of nylon fabric, and one wedge (2) 50 mm wide is made of excelsior fabric, which is a mesh. The wedges are interconnected with a seam "in the lock". On the seams connecting the wedges of the dome, nylon ribbons LTKP-13-70 are stitched. The lower edge of the dome is reinforced on both sides with nylon tape LTKP-15-185. On the lower edge of the dome, all slings, except for slings No. 1A, 1B, 13A, 13B, have jumpers made of nylon tape LTKP-15-185, which are designed to prevent cases of overlapping of the dome with slings and reduce its filling time. On the basis of the canopy, between lines No. 1A and 1B, 13A and 13B there are slots (3) 1.7 m long, designed to turn the canopy during descent. The main parachute (Fig. 1.25) has 26 main lines (1) made of ShKP-150 nylon cord (of which 22 lines are 4 m long and 4 lines (4) are attached to the loops of the canopy slots, 7 m long), 22 are external additional slings (2) 3 m long , as well as 24 internal additional slings (3) from a kapron cord ShKP-120 4 m long.

Additional lines are attached to the main lines, and two additional internal lines (3) are attached to lines No. 2 and 14 (5). The slings are tied at one end to the loops of the dome, at the other - to the half-ring buckles of the free ends (6) of the suspension system.

To facilitate the laying of the main parachute on lines No. 1A, 1B and on an additional line No. 24 at the lower edge of the canopy, as well as at the half-buckles

The arms of the suspension system are sewn with identification sleeves made of green or cotton fabric. of blue color, and on the additional sling No. 12 - red or orange.

To facilitate the laying of lines, they are marked at a distance of 0.2 m from the lower edge of the dome and 0.4 m from the half-ring buckles of the free ends of the suspension system, indicating the beginning and end of laying.

On the lower edge of the dome, to the left of the lines, their serial numbers are indicated. On the outside of the canopy, between lines 1A and 24, there is a factory marking. On slings No. 1A and 13A, 1B and 13B, control lines (4) are sewn (Fig. 1.26) , which are designed to turn the dome and are made of kapron cord ShKKr-190 of red color in two additions. The control lines are threaded through the rings (2) sewn with inside free ends (1) of the suspension system. One end of the left control line is attached to the line

pe No. 13A at a distance of 1.65 m, the second - to the line No. 1A at a distance of 1.45 m from the half-ring buckles of the free ends of the suspension system. One end of the right control line is attached to the line No. 13B at a distance of 1.65 m, the second - to the line No. 1B at a distance of 1.45 m from the half-ring buckles of the free ends of the suspension system.

When tensioning the right control line, lines No. 1B and 13B are pulled, pulling the lower edge of the dome inward. The air flow coming out from under the edge at the place of its hem creates a reactive force that rotates the dome, and it turns to the right (Fig. 1.27).

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When pulling the left control line, lines No. 1A and 13A are pulled and the canopy turns to the left.

suspension system parachute is intended:

For connecting a parachute to a parachutist;

For uniform distribution of the dynamic load on the parachutist's body at the moment of opening the parachute;

For convenient placement of a parachutist in it, for attaching a reserve parachute, weapons and equipment.

The suspension system (Fig. 1.28) is made of LTK-44-1600 nylon tape and consists of the following parts:

Loose ends (1);

Main girth (2);

Back and shoulder girths (3);

Breast jumper (4);

Waist girth (5);

Leg loops (6);

Pinning device (7).

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Loose ends marked with numbers: 1 and 2 - the right pair, 3 and 4 - the left and end with half-ring buckles, to which the main parachute lines are attached. At the free ends, marked with the numbers 2 and 3, there are rubber loops made of elastic tape, designed to fill the slack in the control lines. In the upper part of the free ends, four ribbons with rings are sewn, through which the control lines are passed.

Each pair of free ends has a locking cord made of ShKP-150 cord, which is used when using a parachute system without rolling over the free ends of the harness.

Main Girth stitched from ribbons in two additions. On the left in the upper part of the main girth there are two curved buckles: the lower one for connecting it with the left back-shoulder girth, the upper one for fastening the left pair of free ends.

On the right, in the upper part of the main girth, there are three curved buckles: the lower one for connecting it with the right dorsal-shoulder girth, the upper _ for fastening the link of the pinning device made of the LTKP-43-900 tape and the right detachable pair of free ends, the middle one -

for mounting the link of the pinning device.

FROM reverse side the main girth, below the curved buckles, with the help of the tape LTKrP-43-800, buckles are sewn for fastening the belts of the cargo container.

On the left side of the main girth, below the curved buckles, a LTKkrP-26-600 tape is sewn for attaching a flexible hose, and below, at chest level, a manual opening link pocket is sewn.

To attach the free ends of the intermediate suspension system of the reserve parachute, two fastening brackets are mounted in the main girth.

Below, with the help of tape LTKrP-43-800, buckles are sewn into the main girth for pulling up the knapsack with the help of adjusting tapes. Here, in the triangles formed by the straps of the back-shoulder girths, a carabiner is fixed on the left side, and on the right side there is a buckle for fastening the leg girths. In the lower part, the main girth is bifurcated, the tapes are sewn end-to-end, and they are sewn with a soft pad for comfortable sitting in the suspension system and rings for pulling up the lower corners of the pack.

Back and shoulder girths to exclude spontaneous movement through curved buckles and buckles with toothed bridges, they have LTKkrP-43-800 tapes sewn on them and loops from LTKkrP-43-800 tape.

chest jumper formed by dorsal-shoulder girths going up from the crosspiece through curved buckles, and has a carabiner in the left half, and a buckle in the right.

Leg loops formed by the lower ends of the back-shoulder girths, passed between the ribbons of the main girth, and have a carabiner on the right girth, and a buckle on the left. Rectangular buckles are mounted on the leg loops for adjusting the leg loops according to the height of the parachutist.

Waist girth formed by ribbons of the chest bridge after passing them between the ribbons of the main girth; it has two rectangular adjustment buckles

Pinning device(Fig. 1.30) is designed to disconnect the right pair of free ends from the suspension system and is made of lightweight tape LTKOkr-44-1600, on which are sewn:

Tape LTKMP-12-450, forming a loop to which a pin-check is attached;

Tape LTKP-15-185, forming a loop for fastening the pinning device to the curved buckle of the main girth;

Tape LTKrP-26-600 forming a handle.

A textile fastener is sewn on the ends of the tape LTKOkr-44-1600. A removable parachute honeycomb is fixed on the pin-pin ring.

knapsack(Fig. 1.31) is intended for laying in it the canopy of the main parachute with lines, laid in the chamber, part of the free ends of the harness and placing the device.

The knapsack is made of nylon avisent or nylon fabric and consists of a base, false bottom, right and left flaps. A stiffening frame is inserted between the main and false bottom.

On the right flap there is a pocket of the device made of LTKrP-26-600 tape with tie ribbons and a pocket of the parachute device activation cord made of LTK-44-1600 tape with a valve. Attached to the top of the right flap is a rubber honeycomb for mounting a stacked stabilizing system on top of the pack. On the outside of the right valve there is a handle made of LTKrP-26-600 tape, which is designed to pull the right valve back when filling the slack link of the stabilizing parachute under it in preparation for making a parachute jump from the Il-76 aircraft.

Rings are sewn into the free corners of the right and left valves of the backpack, designed to hold the valves in a tightened state.

A removable honeycomb is mounted on the ring of the right valve, and on the upper part of the satchel, on the outer side of the left valve, a welded ring is sewn on the satchel, designed to secure the removable honeycomb with a tape located on the loop of the parachute link of the stabilizing system.

At the beginning of the stitching of the right flap, a wire ring was sewn with the help of the LTKrP-20-150 tape, designed to lock the fastening loop of the parachute device activation cord. On the same section of the right valve there is a loop with a button spike for the valve covering the two-cone lock. In the upper part of the knapsack, under the fastening plate of the two-cone lock, with the help of the tape LTKrP-20-150, a ring is fixed, designed to pass through the rubber honeycomb, which fastens the stacked stabilizing system on the upper part of the knapsack. FROM opposite side there is a second loop with a button spike for the valve covering the two-cone lock. On the left side of the satchel, one end of a flexible hose is fixed on a buckle with a toothed bridge, which is designed to accommodate the cable of the manual opening link and protect it from accidental snagging (hose length - 0.38 m).

At the top of the stiffening frame there are two round and four oblong holes (Fig. 1.32). In the two upper elongated holes, LTKkrP-43-800 ribbons are fixed, which end with buckles with toothed bridges and are designed to fasten the satchel to the dorsal-shoulder girths of the suspension system. Regulating bands LTKMkrP-27-1200 are fixed in two lower longitudinal holes.

Note: a stiffening frame with two windows at the top is allowed

parts of a backpack. On this satchel there are ribbons ending in yarn

kami with serrated bridges, fixed in the upper

side, and adjusting tapes - at the bottom of the windows.

On the inside of the knapsack at a distance of 0.26 m from the top there is a mark that limits the laying of the free ends on the knapsack.

Based on the knapsack, the following are scribbled:

Eight loops for fastening the backpack to the suspension system;

Two-cone lock valve;

Two scarves.

The kerchiefs are equipped with round buckles with floating bridges, in which LTKkrP-26-600 straps for fastening the reserve parachute are threaded, ending with carbines, and orange ribbons LTKkrP-26-600, which are designed to quickly release the straps for fastening the reserve parachute. On the left scarf there is a pocket for a card that replaces a passport. Above the sewing of the right scarf on the knapsack, two ties are sewn for attaching the device hose. On the lower corners of the knapsack, two pull-up tapes are sewn, made of LTKrP-26-600 tape in two additions and designed to attract the lower corners of the knapsack to the suspension system.

Double cone lock(Fig. 1.33) is designed to hold the buckles of the power tapes of the stabilizing system during stabilization and release them when the manual opening link is pulled out or the parachute device is triggered. The two-cone lock includes the following parts:

Mounting plate;

Housing with two cones;

Shutter with two cones;

Two shock absorbers;

Spring and adjusting washers;

mounting plate;

Cover screw;

5 fastening screws;

W manual opening vein(Fig. 1.34) is designed to open the two-cone lock by the parachutist himself. It consists of a ring made of steel bar; rope 0.6 m long; limiter and wire loop. Cable link manual opening at a distance of 0.21 m from the limiter and 0.057 m from the loop

covered with polyethylene oloch. Manual link allowed

openings without a polyethylene sheath on a cable.

Safety parachute device(Fig. 1.35) is designed to open a two-cone lock in case the skydiver for some reason did not pull out the manual opening link.

____________________________

With parachute system D-10

devices of the type PPK-U-165A-D and AD-3U-D-165 are used with hoses 0.165 m long, cables 0.322 m long, loops 0.019 m long and switching cords 0.36 m long with flexible studs.

parachute bag(Fig. 1.36) is intended for laying the parachute system in it during transportation and storage.

_____________________

Rectangular parachute bag, made of avisent and has: two handles, a loop for a tag, a flap with two half-ring buckles, a cord for tightening the bag, a tag for sealing the bag, a tape for tightening the valve and a pocket.

The passport is an integral part of the parachute system and is designed to keep records of the reception, transfer, securing, maintenance, operation, repair and modification of the parachute system.

To auxiliary parts include safety thread and safety cord SHHB-20.

Safety thread they will lock the loop of the link of the stabilizing system with the ring on the knapsack, the flexible pin in the shutter of the parachute device, the shutter of the two-cone lock.

It is made of cotton yarn (you can use the core of the cord ШХБ-125, ШХБ-60).

Safety cord 0.3 m long, the rings of the stabilizer feathers are hidden with the rings of the camera of the stabilizing system, while when landing from the An-2 aircraft, the Mi-8 helicopter, the ShHB-20 is used in two additions, from the Il-76 aircraft - in one addition.

Parachute D-10

The D-10 landing parachute system is designed for training and combat jumps from the An-22, Il-76, An-26 military transport aircraft, from the An-2 aircraft and Mi-6 and Mi-8 helicopters, performed by individual paratroopers or groups of paratroopers of all specialties with or without full service weapons and equipment with a total flight weight of a paratrooper of 140 kg.

Technical and operational characteristics

Operating restrictions
Weight of a paratrooper with parachutes, kg
Aircraft flight speed, km/h
Maximum safe parachute opening height, m
Minimum safe application height, m
Stabilization time, s
Speed of descent on a stabilizing parachute, m/s
The force required to open a two-cone lock using a manual opening link, kgf	no more than 16
Speed of descent on the main parachute, m/s
Time to turn in any direction by 180 when the lock cord is removed and the free ends of the harness are pulled, s	no more than 60
Time to turn in any direction by 180 with locked free ends of the suspension system, s	no more than 30
Average horizontal forward and backward speed, m/s	not less than 2.6
Height of a paratrooper-paratrooper, m
Weight of parachute system without parachute bag and parachute device AD-3U-D-165, kg,	no more than 11.7
Number of uses:
with a total flight weight of a paratrooper-paratrooper of 140 kg,
including with a total flight weight of a parachutist of 150 kg
Shelf life without repacking, months	no more than 3
Warranty period, years

The D-10 parachute system allows the use of reserve parachutes of the Z-4, Z-5, Z-2 types. Parachute devices AD-3U-D-165, PPK-U-165A-D are used as a safety device for opening a two-cone lock.

Parts of the parachute system

1. Camera stabilizing system;

2. Stabilizing system (stabilizing lineless parachute);

3. Main parachute chamber;

4. Main parachute (dome with lines);

5. Suspension system;

7. Double cone lock;

8. Manual opening link;

9. Safety parachute device type PPK-U or AD-ZU-D;

10. Parachute bag;

11. Passport;

12. Auxiliary parts and details.

Camera Stabilization System

It is intended for laying in it the stabilizing dome with slings and the upper part of the stabilizer, as well as for the orderly activation of the stabilizing system.

The shape is cylindrical. Material - kapron advice. It consists of a base (4) and those on it: in the upper part - a carabiner (1) for attaching to a cable or extension cord in an airplane, a lashing tape (7) for catching a rubber honeycomb, protect, a cord-tie (3) for tightening the camera; at the bottom - metal rings (5) for locking with stabilizer rings.

The stabilizing system (stabilizing slingless parachute) is designed to activate the safety parachute device, ensure a stabilized descent of the parachutist and to open the main parachute.

Stabilizing system

It consists of a canopy with lines and a stabilizer with a parachute link.

The base of the dome (1) has the shape of a truncated cone with a larger base area of 1.5 m2, made of nylon. An exhaust device (2) is sewn onto the dome in the pole part, which is designed to ensure the filling of the dome and consists of eight pockets. Reinforcing tapes are sewn on the outer side of the dome: radial (3) - from the tape LTKP-15-185 and circular (4) from the tape LTKP-13-70. The edge of the dome is reinforced by folding the fabric to the outer side and stitched onto it on both sides with an LTKP-15-185 tape. Along the lower edge of the dome under the radial reinforcing tapes, the ends of 16 slings made of the ShKP-200 cord are threaded and attached in a zigzag stitch. The length of the outer lines (6) in the free state from the lower edge of the canopy to the stabilizer feather is 0.52 m, and the middle lines (5) are 0.5 m. The canopy has a factory stamp (18): parachute index and year of manufacture.

Stabilizer

Serves to prevent rotation of the stabilizing parachute and consists of two feathers (7), each of which is made by DIV_ADBLOCK48">

The triangle formed from the ribbons is closed on both sides with kerchiefs (14) made of nylon advisor. A guide ring (16) is sewn onto the power tapes between the scarves with the help of a tape (15) LTKrP-26-600, through which the parachute device activation cord is passed. On the power tapes near the buckles, arrows are applied with black harmless paint to control the correct installation and installation of power tapes on a two-cone lock.

Parachute stabilizing strapless

It consists of a dome, stabilizer and parachute link. The dome (1) has a hemispherical shape with an area of 1.5 m2 and is made of nylon fabric. Radial reinforcing tapes (3) LTKP-15-185 and circular tapes (2) LTKP-13-70 are stitched on the outer side of the dome. The edge of the dome is reinforced with LTKP-15-185 tape stitched onto it on both sides. The canopy is marked with a factory stamp: parachute index and year of manufacture.

Stabilizer

Serves to prevent rotation of the stabilizing parachute and consists of four feathers (4), which are made of gray nylon fabric. On the surface of each stabilizer feather, on both sides, a reinforcing frame made of LTKP-13-70 tape is sewn. At one end of the lashing tape there is a loop for attaching to the loop of the parachute link of the stabilizing parachute, at the other end there is a mark limiting the lashing.

Main parachute chamber

Serves for laying in it a dome with lines of the main parachute and for its orderly opening. The camera is made of gray nylon fabric and has the shape of a cylinder (when folded).

The surface of the chamber is reinforced with two tapes (2) LTKrP-26-600, which form a bridle in the upper part. For the convenience of laying the dome into the chamber along the upper base of the chamber and the ribbons of the bridle, we have our scarf (5). In the hem of the upper base of the chamber, a cord-tie (3) from the ShKP-150 cord is inserted and attached, which is designed to tighten the upper base of the chamber.

On the base of the camera is sewn:

Reinforcement (12) made of gray nylon fabric;

Nine straight (10) combs with ribbons (11) at the bottom for laying main parachute lines;

Honeycomb spreader (8) with honeycomb rubber (9) from knapsack cord to hold the lines in the comb;

Valve (15) with two pairs of eyelets (14) for passing through removable rubber honeycombs (16, 17) and with two pockets (21) for covering bundles of lines; for the convenience of laying the slings, the valve near the eyelets is marked - 1,2,3,4;

Pocket (22) at the top base of the chamber for threading the ends of the cord-tie.

To cover the bundles of slings laid in honeycombs, aprons (7) made of gray nylon fabric with tie ribbons (6) are sewn in the upper part of the chamber.

A ring (20) made of an elastic band 29 mm wide is inserted into the hem of the lower part of the chamber, designed to ensure an orderly exit of the main parachute canopy from the chamber.

At the lower base of the chamber, two removable rubber honeycombs are installed and an apron (19) is sewn on, which in turn, it has two more removable rubber honeycombs.

main parachute

Designed to ensure a safe rate of descent and landing of a parachutist.

Consists of the base of the dome and lines. The base of the dome consists of 24 wedges (1), which form a non-planar circle with an area of 100 m2. Each wedge of the dome, in turn, consists of seven wedges, six of which are made of nylon fabric, and one wedge (2) 50 mm wide is made of excelsior fabric, which is a mesh. The wedges are interconnected with a seam "in the lock". On the seams connecting the wedges of the dome, nylon ribbons LTKP-13-70 are stitched. The lower edge of the dome is reinforced on both sides with nylon tape LTKP-15-185. On the lower edge of the dome, all slings, except for slings No. 1A, 1B, 13A, 13B, have jumpers made of nylon tape LTKP-15-185, which are designed to prevent cases of overlapping of the dome with slings and reduce its filling time. On the basis of the canopy, between lines No. 1A and 1B, 13A and 13B there are slots (3) 1.7 m long, designed to turn the canopy during descent.

main parachute

It has 26 main lines (1) made of ShKP-150 nylon cord (of which 22 lines are 4 m long and 4 lines (4) are attached to the loops of the dome slots, 7 m long), 22 external additional lines (2) are 3 m, as well as 24 internal additional slings (3) from a kapron cord ShKP-120 4 m long.

Additional slings

They are mounted to the main lines, and two additional internal lines (3) are attached to the lines No. 2 and 14 (5).

The slings are tied at one end to the loops of the dome, at the other - to the half-ring buckles of the free ends (6) of the suspension system.

To facilitate the laying of the main parachute, on lines No. 1A, 1B and on additional line No. 24 at the lower edge of the canopy, as well as on the half-ring buckles of the suspension system, identification sleeves are sewn, made of green or blue cotton fabric, and on additional line No. 12 - red or orange.

To facilitate the laying of lines, they are marked at a distance of 0.2 m from the lower edge of the dome and 0.4 m from the half-ring buckles of the free ends of the suspension system, marking the beginning and end of laying.

On the lower edge of the dome, to the left of the lines, their serial numbers are indicated. On the outside of the canopy, between lines 1A and 24, there is a factory marking.

Lines No. 1A and 13A, 1B and 13B are sewn with control lines (4), which are designed to turn the canopy and are made of red nylon cord ShKKr-190 in two additions. The control lines are passed through the rings (2) sewn on the inside of the free ends (1) of the suspension system. One end of the left control line is attached to line No. 13A at a distance of 1.65 m, the other end is attached to line No. 1A at a distance of 1.45 m from the half-ring buckles of the free ends of the suspension system. One end of the right control line is attached to the line No. 13B at a distance of 1.65 m, the second - to the line No. 1B at a distance of 1.45 m from the half-ring buckles of the free ends of the suspension system.

When tensioning the right control line, lines No. 1B and 13B are pulled, pulling the lower edge of the dome inward. The air flow from under the hem at the hem creates a reactive force that DIV_ADBLOCK49">

The main strap is stitched from ribbons in two additions. On the left in the upper part of the main strap there are two curved buckles: the lower one is for connecting it with the left back-shoulder girth, the upper one is for attaching the left pair of loose ends.

On the right in the upper part of the main strap there are three curved buckles: the lower one is for connecting it with the right back-shoulder girth, the upper one is for fastening the link of the pinning device made of the LTKP-43-900 tape and the right detachable pair of free ends, the middle one is for mounting the link dispensing device.

On the reverse side of the main strap, below the curved buckles, buckles for fastening the cargo container straps are sewn with the help of LTKrP-43-800 tape.

On the left side of the main strap, below the curved buckles, a LTKkrP-26-600 tape is sewn for attaching a flexible hose, and below, at chest level, a pocket for a manual opening link is sewn.

To attach the free ends of the intermediate suspension system of the reserve parachute, two fastening brackets are mounted in the main strap..gif" align="left" width="192" height="245">DIV_ADBLOCK51">

It is intended for laying in it the canopy of the main parachute with lines laid in the chamber, part of the free ends of the harness and placing the device.

The knapsack is made of nylon avisent or nylon fabric and consists of a base, false bottom, right and left flaps. A stiffening frame is inserted between the main and false bottom.

On the right valve there is a pocket of the device made of LTKrP-26-600 tape with tie ribbons and a pocket of the parachute device activation cord made of LTK tape with a valve. Attached to the top of the right flap is a rubber honeycomb for mounting a stacked stabilizing system on top of the pack. On the outside of the right valve there is a handle made of LTKrP-26-600 tape, which is designed to pull the right valve back when filling the slack link of the stabilizing parachute under it in preparation for making a parachute jump from the Il-76 aircraft.

Rings are sewn into the free corners of the right and left valves of the backpack, designed to hold the valves in a tightened state.

In the upper part of the knapsack, under the fastening plate of the two-cone lock, with the help of the tape LTKrP-20-150, a ring is fixed, designed to pass through the rubber honeycomb, which fastens the stacked stabilizing system on the upper part of the knapsack. On the opposite side, there is a second loop with a button spike for a valve that covers a two-cone lock. On the left side of the satchel, one end of a flexible hose is fixed on a buckle with a toothed bridge, which is designed to accommodate the cable of the manual opening link and protect it from accidental snagging (hose length - 0.38 m).

Up on ra Me stiffness there are two round and four oblong holes. In the two upper elongated holes, LTKkrP-43-800 ribbons are fixed, which end with buckles with toothed bridges and are designed to fasten the satchel to the dorsal-shoulder girths of the suspension system. In the two lower longitudinal holes, LTKMkrP regulating tapes are fixed.

Note: a stiffening frame with two windows in the upper part of the backpack is allowed. On this satchel, tapes ending in buckles with serrated bridges are fastened on the upper side, and adjusting tapes on the lower side of the windows.

On the inside of the knapsack at a distance of 0.26 m from the top there is a mark that limits the laying of the free ends on the knapsack.

Based on the knapsack, the following are scribbled:

Eight loops for fastening the backpack to the suspension system;

Two-cone lock valve;

Two scarves.

Two pull-up tapes are sewn on the lower corners of the knapsack, made from LTKrP-26-600 tape in two additions and designed to pull the lower corners of the knapsack to the hanging one https://pandia.ru/text/78/403/images/image015_17.jpg" align ="left" width="182 height=127" height="127"> vaniya, operation, repair and completion of the parachute system.

Auxiliary parts include safety thread and safety cord ШХБ-20. The loop of the link of the stabilizing system with the ring on the knapsack, the flexible pin in the shutter of the parachute device, the shutter of the two-cone lock are hidden with a locking thread.

It is made of cotton yarn (you can use the core of the cord ШХБ-125, ШХБ-60).

With a safety cord 0.3 m long, the rings of the stabilizer feathers are hidden with the rings of the camera of the stabilizing system, while when landing from the An-2 aircraft, the Mi-8 helicopter, the ShHB-20 is used in two additions, from the Il-76 aircraft - in one addition.

Airborne parachute systems

Array ( => 257 [~ID] => 257 => 6 [~IBLOCK_ID] => 6 => d-10 [~CODE] => d-10 => 257 [~XML_ID] => 257 => Parachute system airborne D-10 [~NAME] => Airborne parachute system D-10 => Y [~ACTIVE] => Y => [~DATE_ACTIVE_FROM] => => [~DATE_ACTIVE_TO] => => 500 [~SORT] = > 500

Description

S domes - 100 m²;

parachutist weight 120 kg;

Service life - 14 years;

GK-30 and GK-30-U;

165A-D or link r / r;

bags and PPK-U device.

[~PREVIEW_TEXT] =>

The parachute landing system "D-10" is designed to perform single and group jumps

from military transport aircraft and helicopters equipped for landing.

Description

Characteristics of the parachute system "D-10":

S domes - 100 m²;

Rate of descent - no more than 5 m / s from the flight

parachutist weight 120 kg;

Service life - 14 years;

Possibility of attaching a cargo container

GK-30 and GK-30-U;

The system is put into action by the PPK-U device

165A-D or link r / r;

System weight - no more than 11.7 kg without portable

bags and PPK-U device.

System (with the total flight weight of the parachutist

140 kg) ensures reliable work at height

200-4,000 m with 3 second stabilization

and more when leaving the aircraft at speed

38.9–111.1 m/s (140–400 km/h).

JSC Polet Ivanovo Parachute Plant is the only serial manufacturer in Russia of a wide range of parachute equipment for human use. The enterprise has state licenses for all types of activities related to the development, production and disposal of parachutes.

PARACHUTE D-10

PARACHUTE OF D-10

08.06.2013
NEW PARACHUTES HAVE BEEN IN SERVICE IN THE AIR AND STORM UNION OF THE SOUTH VO

Guardsmen of the air assault unit of the Southern Military District (SMD), stationed in the Volgograd region, have begun to master the new D-10 parachutes, which entered service with the unit this year.
The personnel were trained on the device of a new parachute and the order of its laying, training at the airborne complex, after which the military personnel began to carry out landing on the sites training center"Lebyazhye" in the Volgograd region.
The landing of military personnel is carried out from the Il-76 military transport aircraft, as well as from the latest helicopters army aviation Mi-8 AMTSh "Terminator" from a height of 800 m.
Press Service of the Southern Military District

18.10.2013
Federal agency for the supply of weapons, military, special equipment and material resources, acting in the interests of the Ministry of Defense of the Russian Federation, announced an electronic auction for the supply of 3,300 D-10 parachute systems.
According to the press service of Rosoboronpostavka, the military department is ready to pay no more than four hundred and six million thirty-five thousand three hundred rubles for the entire set.
The D-10 parachute system is designed for combat and training jumps in the altitude range from 200 to 4000 m at a flight speed of 140 to 400 km/h with stabilization for 3 seconds, with a total parachutist flight weight of 140 kg.

22.10.2013

The Scientific Research Institute of Parachute Engineering (Research Institute of Parachute Engineering), which is part of the Aviation Equipment holding of the State Corporation Rostec, will present an experimental model of a modified parachute -landing system (PDS) D-10P.

30.11.2013
The new special parachute D-10P from JSC Research Institute of Parachute Building of the Aviation Equipment holding is designed to perform special tasks and provide emergency assistance. For the first time, the new parachute landing system (PDS) D-10P was demonstrated in the air at MAKS-2013. A little later, it was shown to the audience at the International Exhibition of State Security Means "Interpolitech-2013". The new system allows you to drop troops from a height of 70 meters when an aircraft or helicopter exits from an attack by a ground enemy.
Research Institute specialists began work on the creation of the system in 2011, and already in 2012 they successfully tested it with mannequins and people. With sufficient process assurance, testing can be completed within 2-3 months. as potential customers new system special forces of Russian and foreign law enforcement agencies and rescuers are considered.
Rostec

05.06.2014
The Airborne Forces (VDV) received more than 1.7 thousand D-10 parachutes at their disposal. The largest batch of new parachutes of the tenth series entered the Kamyshin Airborne Forces unit. In addition, the Tula, Ulan-Ude and Ussuri formations received new parachute systems, the press service and information department of the Russian Defense Ministry reported.
Parachutes D-10 are delivered in airborne units to replace obsolete parachute systems D-6 (4th series) or worn-out parachutes.

09.09.2016
The Technodinamika holding of the Rostec State Corporation will start developing modified D-10 parachutes, one of the most popular parachutes currently in service with the Airborne Forces. The terms of reference for the new parachute system have already been prepared, and development work will begin in 2017.
Parachutes D-10, which are currently used in the Airborne Forces, will be modernized. The work will be carried out by the main developer of parachute technology in Russia, the Scientific Research Institute of Parachute Engineering (part of the Technodinamika holding of the Rostec State Corporation). On the this moment terms of reference for a new parachute system have been developed, development work will begin in 2017.
“Modernization of the D-10 series 2 parachute will involve the development of a harness system with improved ergonomics, which, among other things, can be combined with modern equipment sets, such as the Ratnik, and the placement of a cargo container in front under the reserve parachute. — Tells CEO"Technodynamics" Maxim Kuzyuk. “The cargo container will allow the paratroopers to get more autonomy when performing combat operations, in addition, in the event of a splashdown of a paratrooper, it will be used as a raft.”
The D-10 series 2 system is designed for jumping from Il-76, An-2 and Mi-8 helicopters by paratroopers of all specialties with full service weapons and equipment (or without it), as well as by individual paratroopers or groups of paratroopers.
Holding "Technodinamika"

09.11.2016

Serbian special forces units adopted Russian D-10 parachutes donated by the commander of the Russian Airborne Forces, the brigade commander told reporters on Tuesday special purpose Serbian Armed Forces Brigadier General Zoran Velickovic.
The international tactical exercises "Slavic Brotherhood 2016" are held from November 2 to 15 near Belgrade, units of the armed forces of Russia, Belarus and Serbia take part in them. About 200 Russian servicemen are involved in the exercises.
“Last year, we received a batch of D-10 parachutes as a gift from the commander of the Airborne Forces, and just recently they were put into service,” Velichkovich said at the exercises.
RIA News

03.05.2017
The D-10 parachute for the Ratnik combat gear will be upgraded by 2018, Colonel-General Andrey Serdyukov, commander of the Russian Airborne Forces, said on Friday.
On Friday, a solemn ceremony was held in Ulyanovsk to hand over a set of the latest BMD-4M combat vehicles and Rakushka armored personnel carriers to servicemen of the 31st Separate Guards Air Assault airborne brigades. In the presence of the commander of the troops, about 50 units of equipment were transferred to the formation.
“In 2018, it is planned to carry out development work to modernize the D-10 landing parachute system and a reserve parachute for landing personnel in the Ratnik combat set,” Serdyukov said.
He clarified that in 2018 it is also planned to complete development work to create a whole line of multi-purpose platforms and parachute-cargo systems for landing weapons, military equipment and cargo with a flight weight of 500 kilograms to 18 tons.
RIA News

28.10.2017

By the end of the year, the airborne troops will have at their disposal more than 10,000 sets of D-10 parachute systems.
Their next batches are already in the Tula, Ivanovo, Pskov, Novorossiysk, Ulan-Uda and Ussuriysk formations of the Airborne Forces, where military personnel actively use them in the process of combat training.
New D-10 parachutes are coming to the Airborne Forces units to replace the old systems that have exhausted their resources.
They are designed to perform combat and combat training jumps from military transport aircraft (VTA) at flight speeds from 140 to 400 km/h at altitudes up to 4000 m.
The D-10 parachute is used in the Airborne Forces for the mass landing of military personnel and is simpler and safer in comparison with other parachute systems.
The area of the dome of the new parachute is 100 square meters. meters, and its special shape makes it easy to turn around in the wind.
Parachutes D-10 have increased service life and service life.
Department of Information and mass communications Ministry of Defense of the Russian Federation

26.11.2017
All divisions marines The Russian Navy is equipped with the new D-10 parachutes, which replaced the D-6 system, the Deputy Commander-in-Chief said on the air of the Ekho Moskvy radio station on Saturday Navy(Navy) Russian Lieutenant General Oleg Makarevich.
The Day of the Marine Corps of the Russian Navy (created in 1705 during the Northern War with Sweden) is celebrated annually in the Russian Federation on November 27.
“Practically all Marine Corps units are already equipped with these parachutes,” Makarevich said. According to him, the reconnaissance units of the Marine Corps Russian fleet equipped with special parachutes.
The Deputy Commander of the Russian Navy noted that in 2017, Russian marines made more than 10,000 parachute jumps.
"Since 2012
RIA News

06.03.2018
Modernization of the D-10 parachute system and the Z-5 reserve parachute for landing personnel Airborne Troops Russia in the Ratnik combat kit will begin in March, said the head of airborne training - deputy commander of the Airborne Forces for airborne training Vladimir Kochetkov.
“As for human parachutes, in March of this year, the Renovation development work will open to modernize the D-10 parachute system and the Z-5 reserve parachute for landing personnel in the Ratnik combat kit,” Kochetkov said in an interview with the Russian newspaper. armed forces "Red Star".
According to him, now the Russian Airborne Forces use the D-6 series 4 and D-10 parachute systems for landing personnel; reserve parachute Z-5, special-purpose parachute systems "Crossbow-1" and "Crossbow-2"
RIA News

PARACHUTE D-10

The D-10 parachute replaced the D-6, which is in service, is simpler and safer when landing and in operation. The volume of the dome of the new parachute is 100 square meters. m instead of 83 sq. m from its predecessor, its rounded shape ensures a smooth landing.
The D-10 is designed to carry out combat and training jumps at flight speeds from 140 to 400 km/h with stabilization for 3 seconds, in the altitude range from 200 to 8000 m. jumping conditions. The mass of the new parachute is several kilograms less than the mass of its predecessor, which makes it easy to turn in the wind, perform horizontal glide, you can jump into the water with it and quickly extinguish the canopy in strong winds.
Designed to perform single and group training and combat jumps from any aircraft and helicopters at speeds from 140 to 400 km/h.
It is used with a Z-5 reserve parachute.
The system has increased performance when paratroopers descend in the air on filled canopies of the main parachutes.
The application scheme provides for stabilization with subsequent activation of the parachute by a manual deployment link or by the PPK-U 165-AD device. For an exception, it was dragged along the ground, after landing in a strong wind, uncoupling of one free end of the suspension system is provided.

PARACHUTE SYSTEM D-10 SERIES 2

Designed to perform single training and combat jumps, as well as group jumps from any military transport aircraft and helicopters. It is used with reserve parachutes Z-2 or Z-5.
The system has increased performance when paratroopers descend in the air on filled canopies of the main parachutes.
The system is put into operation by the PPK-U-165A-D or AD-ZU-D-165 device with a hose length of 0.165 m or a manual opening link.
The canopy of a non-flat round parachute with an area of 100 m2 provides a vertical descent speed of up to 5 m/s with a paratrooper flight weight of 120 kg. The dome uses Excelsior mesh fabric.
For an exception, it was dragged along the ground, after landing in a strong wind, uncoupling of one free end of the suspension system is provided.
Manufacturer: OAO Polet - Ivanovo Parachute Plant.

Specifications
Range applications	height 200 - 4000 m, speed 140 - 400 km/h