DRONE PARACHUTE SYSTEMS

for UAVs ranging from 5kg to 1000 kg. These systems are designed for deployment at speeds between 20km/h and 220km/h, extension feasible

OVERVIEW

UAVOS' family of parachute systems has been specially designed both for UAV recovery and as a safety measure that can be used in case of UAV catastrophic failure.

UAVOS parachutes benefit from an automatic cord-cutter system that releases the parachute once the air vehicle has landed, minimizing the potential for damage due to high wind.

Hand-sewn from high-grade parachute materials, the parachutes feature a variety of designs that offers the best compromise between packed volume and parachute drag coefficient, providing a safe and low-impact landing for your drones and payloads. The system has been thoroughly tested on UAVOS' drones.

FEATURES

Key advantages of UAVOS’ Drone Parachute Systems are:

  • High speed-range for initial phase of deployment: 20km/h to 220km/h tested, extension feasible
  • Moderate G-load throughout total deployment-range due to configurable slider system: standard <6g
  • Quick stabilization after deployment
  • Low tendency of oscillation
  • Extreme low weight and dimensions resulting in low effect on payload: standard 1.5-2.0kg with 4-6.5 liter volume
  • Re-useable: 10+ deployments possible
  • Development and production in accordance with aeronautical engineering regulations
  • Verification of required parameters through special measuring equipment and video documentation during airdrop-tests
  • Low adaptation and development efforts while in design phase to consider specific requirements.

SPECIFICATIONS


Picture


RS name

Cell

10 System of Standard Parachute Landing

10 Parachute Systems

15 Parachute Systems

25 Parachute Systems

50 System of Standard Parachute Landing

50 Parachute Systems

UAV type (aircraft, helicopter, multi-rotor)

type

airplane

airplane / helicopter / multi-rotor

airplane / helicopter / multi-rotor

airplane / helicopter / multi-rotor

airplane

airplane / helicopter

RS type (standard, accident, emergency)

type

standard

standard / emergency

standard / emergency

standard / emergency

standard / emergency

standard / emergency

Commissioning principle (self-extracting, ballistic, ballistic-exhaust)

type

self-extracting

ballistic

ballistic

ballistic

self-extracting

ballistic-exhaust

Type of the pilot chute (exhaust, brake, stabilizing)

type

stabilizing

-

-

-

exhaust / brake / stabilizing

exhaust / brake / stabilizing

The number of attachment points for the lanyard on the UAV

pcs

4

1

1

1

1-4

1

Maximum allowable load

kg

15

15

20

35

60

60

The maximum speed of the UAV when the RS is triggered, without a braking parachute

m/s

up to 16

up to 33.3

up to 20

up to 33.3

up to 33.3

up to 33.3

The maximum speed of the UAV when the RS is triggered, with a braking parachute

m/s

-

-

-

-

up to 300

up to 300

The maximum speed of the UAV when the RS is triggered

km/h

20

0

0

0

5

5

Min. RS response time

s

3

2

1

3

3

2

Minimum altitude when the RS is triggered at minimum speed

m

50

50

10

50

50

50

Operating temperature

°С

-20°С/+30°С

-40°С/+50°С

-40°С/+50°С

-40°С/+50°С

-20°С/+30°С

-40°С/+50°С

Technical resource of the parachute, number of applications

times

50

30

30

30

30

10

Technical resource of the charge

times

-

1

1

1

-

1

Technical resource of the cartridge tube

times

-

3

3

3

-

3

Service life

Mos.

12

12

12

12

12

12

Overall dimensions LxWxH of the parachute compartment

mm

300x120x40

142x130x130

100x100x180

136x136x175

260x220x80

260x220x80

Overall dimensions LxWxH of the ballistic compartment

mm

-

-

-

--

-

214x80x70

Weight

kg

0.3

0.8

0.7

1.3

2,5

3

Maximum overload with max. Load

g

1.2

6

6

6

6

6

Descent rate with max. Loading

m/s

up to 4

up to 6

up to 6

up to 6

up to 6

up to 6

Slider

Cell

no

no

no

no

yes

no

Container type (soft/hard)

soft/hard

-

hard

hard

hard

soft/hard

soft/hard

Actuation

Cell

-

application of power supply

application of power supply

application of power supply

-

application of power supply

Operating supply voltage

V

-

5

5

5

-

5

Operating current of charge actuation, not less

mA

-

500

500

500

-

500

Possibility to install a lock

No.

No. 1

No. 2 - No. 3

No. 2 - No. 3

No. 2 - No. 3

No. 3

No. 3

Square

6.3

6.5

7

15

35

35

Repacking interval

Days

60

60

60

60

60

60

Picture


Cell

RS name

Cell

75 System of Standard Parachute Landing

75 Parachute Systems

100 Parachute Systems

200 Parachute Systems

350 Parachute Systems

1000 System of Standard Parachute Landing

UAV type (aircraft, helicopter, multi-rotor)

type

airplane

airplane

airplane / helicopter

airplane / helicopter

airplane / helicopter

airplane

RS type (standard, accident, emergency)

type

standard / emergency

standard / emergency

emergency

emergency

emergency

emergency

Commissioning principle (self-extracting, ballistic, ballistic-exhaust)

type

self-extracting

ballistic-exhaust

ballistic-exhaust

ballistic

ballistic

ballistic-exhaust

Type of the pilot chute (exhaust, brake, stabilizing)

type

exhaust / brake / stabilizing

exhaust / brake / stabilizing

exhaust / brake / stabilizing

-

-

exhaust / brake / stabilizing

The number of attachment points for the lanyard on the UAV

pcs

1-4

1-4

1

1-4

1

1-4

Maximum allowable load

kg

80

80

120

220

360

1300

The maximum speed of the UAV when the RS is triggered, without a braking parachute

m/s

up to 10

up to 33,3

up to 33,3

up to 97

up to 97

up to 100

The maximum speed of the UAV when the RS is triggered, with a braking parachute

m/s

up to 300

up to 300

up to 110

-

-

up to 300

The maximum speed of the UAV when the RS is triggered

km/h

20

20

5

0

0

50

Min. RS response time

s

1.5

1.5

3

3

4

5

Minimum altitude when the RS is triggered at minimum speed

m

70

70

80

50

200

500

Operating temperature

°С

-20°С/+30°С

-40°С/+50°С

-40°С/+50°С

-40°С/+50°С

-40°С/+50°С

-50°С/+60°С

Technical resource of the parachute, number of applications

times

30

10

10

10

10

5

Technical resource of the charge

times

-

1

1

1

1

1

Technical resource of the cartridge tube

times

-

3

3

-

-

3

Service life

Mos.

12

12

12

12

12

12

Overall dimensions LxWxH of the parachute compartment

mm

300x240x80

300x240x80

350x300x100

300x300x275

210x210x510

х

Overall dimensions LxWxH of the ballistic compartment

mm

-

214x80x70

214x80x70

-

-

х

Weight

kg

2.7

3

3.5

4.5

5.7

х

Maximum overload with max. Load

g

12

12

10

5

5

16

Descent rate with max. Loading

m/s

up to 6

up to 6

up to 6

up to 6

up to 6

up to 6

Slider

Cell

no

no

no

yes

yes

yes

Container type (soft/hard)

soft/hard

soft

soft

soft

hard

hard

hard

Actuation

Cell

-

power supply

power supply

 power supply

power supply

power supply

Operating supply voltage

V

-

5

5

5

5

5

Operating current of charge actuation, not less

mA

-

500

500

500

500

500

Possibility to install a lock

No.

No. 3

No. 3

-

-

-

-

Square

35

35

42

0

56

280

Repacking interval

Days

60

60

60

60

60

60

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