Separation Systems

10 Separation Systems for Space Applications from 5 manufacturers listed on SatNow

Separation Systems for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

Description:The separation system is intended to fasten a microsatellite to the launch vehicle, to separate it and then to move it away. The separation system uses an hermetic expansible tube, four to ten springs...
Satellite Type:
MicroSat, SmallSat
Payload Capacity:
100 Kg
Total Mass:
3.5 to 4.2 Kg
Separation Time:
0.002 sec
Separation Velocity:
1 to 3 m/sec
Payload Side Interface:
12 M6 screws over a 298 mm diameter
Operating Temperature:
-90 to +100 Deg C
Dimension:
348 mm (diameter), 91 mm (height)
more info
Description:The Mark II Motorized Lightband (MLB) is the original in motorized vehicle separation systems. It boasts a heritage of perfect flight under every condition imaginable. From standard sizes to highly cu...
Total Mass:
1.48 to 6.84 Kg
Space Heritage:
Yes
Operating Temperature:
-54 to +128 Deg C
Dimension:
203.2 to 985.774 mm (diameter)
more info
Description:Fully resettable, Low shock, non-pyro technic, non-consumable and debris-free separation system
Payload Capacity:
10 Kg
Total Mass:
2 Kg
Separation Time:
0.025 sec
Separation Velocity:
1 to 1.5 m/sec
Supply Voltage:
22 to 28 V
Space Heritage:
Yes
Operating Temperature:
-15 to +70 Deg C
Dimension:
224 × 209 × 91 mm
more info
Description:SAU&RON also allows customization on the separation velocity to meet customer's requirements on the precise deployment of payloads, making it ideal for critical LEO and interplanetary missions
Satellite Type:
SmallSat
Payload Capacity:
450 Kg
Total Mass:
0.4 (flyaway mass) to 2.3 Kg
Separation Time:
0.15 sec
Separation Velocity:
0.02 to 0.4 m/sec
Supply Voltage:
28 V
Payload Side Interface:
24 x 1/4 inch bolts, according to 15 inch ESPA int...
Rocket Side Interface:
24 x 1/4 inch bolts, according to 15 inch ESPA int...
Dimension:
381 mm (diameter), 30.8 mm (stack height)
more info
Description:CarboNIX uses patented shock-free technology to reduce the risk of damaging sensitive satellites optical payloads and electronic components
Satellite Type:
Microsat
Payload Capacity:
10 to 500 Kg
Total Mass:
330 g (flyaway mass) to 2.6 Kg
Space Heritage:
Yes
Dimension:
203.2 mm (diameter), 381 mm (diameter), 609.6 mm (...
more info
Description:The Advanced Lightband (ALB) is an innovative, lightweight, and compact mechanical separation system used to separate spacecrafts from launch vehicles on orbit. The Advanced Lightband has never failed...
Total Mass:
2.03 to 4.98 Kg
Supply Voltage:
24 to 32 V
Space Heritage:
Yes
Operating Temperature:
-40 to +90 Deg C
Dimension:
203.2 to 609.6 mm (diameter)
more info
Description:Pyro thruster based, compact and debris free release system
Payload Capacity:
35 Kg
Total Mass:
2.5 Kg
Separation Time:
0.01 sec
Separation Velocity:
1 m/sec
Space Heritage:
Yes
Operating Temperature:
-15 to +70 Deg C
Dimension:
170 × 280 × 60 mm
more info
Description:Pyro thruster based, compact and debris free release system
Payload Capacity:
150 Kg
Total Mass:
4.5 Kg
Separation Time:
0.01 sec
Separation Velocity:
1 to 1.2 m/sec
Space Heritage:
Yes
Operating Temperature:
-15 to +70 Deg C
Dimension:
258 × 351 × 91 mm
more info
Description:Release by redundant bolt cutters and system preload can be varied to cater to different satellite inertial properties
Payload Capacity:
2300 Kg
Separation Time:
0.01 sec
Space Heritage:
Yes
Operating Temperature:
-15 to +60 Deg C
Dimension:
937 mm (diameter)
more info
Description:Release by redundant bolt cutters and system preload can be varied to cater to different satellite inertial properties
Payload Capacity:
4000 Kg
Separation Time:
0.01 sec
Space Heritage:
Yes
Operating Temperature:
-15 to +60 Deg C
Dimension:
1194 mm (diameter)
more info


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Space Heritage