Key highlights
ATLAS – release actuators for acceleration of development of new space mechanisms. Tired of complicated and very expensive refurbishment of legacy non-explosive release actuators?
Representative ATLAS can substitute the legacy actuators for the most of the campaign and can be easily refurbished without disassembly under 1 minute at fraction of the cost.
ATLAS is suitable for any development of space mechanism with release nuts of suitable size. Maximal benefits are achieved especially for demanding ECSS qualifications with many releases of multiple HDRMs where use of ATLAS can reduce cost and time by more than 70%.
ATLAS family includes user friendly control electronics and control software.
Fully ECSS flight qualified ATLAS ORBITAL coming in 2027.
Applications
- Solar array HDRMs
- Antenna/boom HDRMs
- Satellite four point separation mechanisms
- Releasable launch locks for payload gimbals and other steerable mechanisms
- Small launcher stage separation
Key features
- Release preload: 1-22 kN
- Actuation: Current pulse
- Release time: <50 ms with ATLAS control electronics (ICU) @ 7A
- Suitable for use in mechanisms requiring precise synchronization
- Reset: User reset within 1 minute with supplied stand without disassembly
- Conditions: laboratory conditions, static loads. Contact us in case of demanding conditions (Fully ECSS flight qualified ATLAS ORBITAL coming in 2027)
- Life: High life, more than 200 releases tested
Customization
- User customizable mechanical interface plate
- User customizable release bolt thread
Manufacturing
- ATLAS is fully manufactured in the Czech Republic (EU)
Testing & qualification
- Extensively tested for laboratory conditions
- Full ECSS qualification ongoing (ATLAS ORBITAL coming in 2027).
Export control
- Available in EU, other countries upon request
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Last updated: 2026-07-22
ATLAS non-explosive release nuts 22kN
list price: 9100 € for single unmodified unit, contact us for reduced pricing of batches
lead time: Starting at 4 weeks, dependent on the batch size, number of initiators and requested modifications.
MOQ: 1
Technical specs
22 kN (maximal release preload)
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