Attach and Release Mechanisms

20 Attach and Release Mechanisms for Space Applications from 5 manufacturers listed on SatNow

Attach and Release Mechanisms 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:Hold Down and Release Mechanism for Satellite Deployment
Space Heritage:
Yes
Mass:
70 g
Current:
4 A (Actuation)
Resistance:
1.2 to 2 Ohm (Fuse Wire)
Proof Load Rating:
7600 N
Release Load Rating:
6000 N
Maximum Angular Misalignment:
6 Degrees
Output Shock:
300 g
Release Time:
50 ms
Operating Temperature:
-135 to 135 Degree C
Dimension:
Ø31.8 x 28 mm
Application:
Antennas, Reflectors, Solar Arrays, Deployable Radiators, Booms, Masts, Scientific Instruments, Satellite and Spacecraft Deployment, Launch Vehicle, M...
more info
Space Heritage:
Yes
Mass:
520 g
Current:
5 A
Output Shock:
100 g
Release Time:
100 ms
Operating Temperature:
-54 to 71 Degree C
Dimension:
66 x 91 x 51 mm
Application:
Spacecraft Hold Down and Release (HDRM) applications, Dispenser/adapter systems, Smaller launch vehicle staging
more info
Description:Ariane Booster Attachment and Separation Mechanism
Mass:
105 to 190 Kg
Flight Limit Load:
507000 N
Separation Time:
0.005
more info
Description:Small Satellite Release Mechanism
Mass:
26 g
Current:
2.7 A (Actuation)
Resistance:
0.5 Ohm
Flight Limit Load:
13 to 1334 N
Operating Temperature:
-20 to 55 Degree C
Dimension:
69 x 38 x 5 mm
Application:
Solar Arrays, Sun Shades, Radiators, Antennas, Booms
more info
Description:Secure and Release Mechanism
Mass:
89 to 95 g
Flight Limit Load:
1500 N
Operating Temperature:
-80 to 80 Degree C
Dimension:
63 x 58.5 x 17 mm
Application:
Solar Arrays, Antennas, Sun Shades
more info
Description:Hold Down & Release Mechanism for Satellites
Space Heritage:
Yes
Mass:
130 g
Current:
4 A (Actuation)
Resistance:
1.2 to 2 Ohm (Fuse Wire)
Proof Load Rating:
22200 N
Release Load Rating:
17800 N
Maximum Angular Misalignment:
6 Degrees
Output Shock:
500 g
Release Time:
50 ms
Operating Temperature:
-135 to 135 Degree C
Dimension:
Ø43.2 x 39.4 mm
Application:
Antennas, Reflectors, Solar Arrays, Deployable Radiators, Booms, Masts, Scientific Instruments, Satellite and Spacecraft Deployment, Launch Vehicle, M...
more info
Space Heritage:
Yes
Mission:
SMART-1, Falconsat-1, STPSat-1, P-POD, CGNSS, CNOFS, XSS-10
Mass:
270 g
Current:
2.3 to 7 A
Resistance:
3.9 Ohm
Power Consumption:
45 W
Maximum Angular Misalignment:
±1.5 Degrees
Output Shock:
400 g
Release Time:
15 to 200 ms
Operating Temperature:
-45 to 75 Degree C
Storage Temperature:
-80 to 75 Degree C
Application:
Spacecraft-from-launch vehicle separation, Solar Array Hold-down and release, Gimbal launch locks and other satellite applications requiring a low-sho...
more info
Description:Ariane Booster Attachment and Separation Mechanism
Mass:
72 to 75 Kg
Flight Limit Load:
2700000 N
Rotational Angle:
±2 Degrees
more info
Description:Secure and Release Mechanism
Mass:
5 g
Flight Limit Load:
50 N
Operating Temperature:
-80 to 80 Degree C
Dimension:
14.5 x 7 x 2.5 mm
Application:
Solar Arrays, Antennas, Sun Shades
more info
Description:Hold Down and Release Mechanism for Satellites
Space Heritage:
Yes
Mass:
200 g
Current:
4 A (Actuation)
Resistance:
1.2 to 2 Ohm (Fuse Wire)
Proof Load Rating:
41000 N
Release Load Rating:
35000 N
Maximum Angular Misalignment:
6 Degrees
Output Shock:
750 g
Release Time:
50 ms
Operating Temperature:
-135 to 135 Degree C
Dimension:
Ø48.3 x 40.6 mm
Application:
Antennas, Reflectors, Solar Arrays, Deployable Radiators, Booms, Masts, Scientific Instruments, Satellite and Spacecraft Deployment, Launch Vehicle, M...
more info

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