Separation Systems

22 Separation Systems for Space Applications from 6 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 (≤ 100 kg) to the launch vehicle, to separate it and then to move it away (Vz ≈ 1 to 3 m/s)
Satellite Type:
MicroSat
Total Mass:
3.5 to 4.2 Kg
Separation Time:
0.002 Sec
Separation Velocity:
1 to 3 m/s
Operating Temperature:
-90 to 100 Degree C
Dimension:
348 mm (Dia), 91 mm (H)
Application:
Hermetic expansible tube
more info
Description:A Broad range of Separation Systems, spanning diameters from 360mm to 2624mm (14” to 103”)
Total Mass:
3.7 Kg, 0.98 Kg (Separated Mass)
Payload Side Interface:
24 x 1/4 inch bolts placed on a diameter of 381 mm...
Rocket Side Interface:
24 x 1/4 inch bolts placed on a diameter of 381 mm...
Space Heritage:
Yes
Dimension:
79 mm (Height)
more info
Description:Separation systems for commercial, government, private and university, LEO, GEO and interplanetary orbits, space flight hardware
Payload Capacity:
200 Kg
Total Mass:
3000 Kg
Separation Velocity:
0.356 m/s
Supply Voltage:
27 V
Space Heritage:
Yes
Operating Temperature:
-40 to 90 Degree C
Application:
Addendum, point in the x direction
more info
Description:Small satellites that require a standard and reliable 15" interface to a launch vehicle
Satellite Type:
SmallSat
Payload Capacity:
450 Kg (260 mm CG height from rocket plane)
Total Mass:
2.3 Kg
Separation Time:
0.015 to 0.025 Sec
Separation Velocity:
0.02 to 0.4 m/s
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...
Space Heritage:
Yes
Application:
ESPA
more info
Description:Non-Pyro Dispenser For 1 Kg Class Nano Satellite
Satellite Type:
NanoSat
Total Mass:
1 Kg
Separation Time:
5 Sec
Separation Velocity:
1 m/s
Supply Voltage:
2.4 V
Space Heritage:
Yes
Operating Temperature:
0 to 60 Degree C
Dimension:
100 x 100 x 113.5 mm
more info
Description:Scalable separation system that is available in sizes of 8", 15" and 24" diameter for microsatellites
Satellite Type:
MicroSat
Total Mass:
10 to 500 Kg
Space Heritage:
Yes
Application:
Electronic components
more info
Description:Range of Separation Systems, spanning diameters from 360 mm to 2624mm (14” to 103”).
Total Mass:
7.2 Kg, 1.9 Kg (Separated Mass)
Space Heritage:
Yes
Dimension:
123 mm (Height)
more info
Description:Separate space vehicles from launch vehicles and to separate elements of launch vehicles, a range of sizes from 8.000 to 38.810 inch bolt circle diameter
Satellite Type:
CubeSat, NanoSat, SmallSat
Payload Capacity:
200 Kg
Total Mass:
3000 Kg
Separation Velocity:
0.356 m/s
Supply Voltage:
28 V
Space Heritage:
Yes
Operating Temperature:
35 Degree C
Application:
Point in the x direction
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:Non-Pyro Dispenser For 2 Kg Class Nano Satellite
Satellite Type:
NanoSat
Total Mass:
2 Kg
Separation Time:
5 Sec
Separation Velocity:
1.5 to 1.9 m/s
Supply Voltage:
2.4 V
Space Heritage:
Yes
Operating Temperature:
0 to 65 Degree C
Dimension:
100 x 100 x 227.5 mm
more info

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Space Heritage