CarboNIX NEO
Compiled from public sources on 2026-05-28. Not independently verified by Exolaunch.
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Off-the-shelf microsatellite separation system using the CarboNIX lock and pusher-arm architecture with a clamp-ring interface for larger satellite masses.
CarboNIX NEO is an Exolaunch shock-free microsatellite separation system for orbital deployment hardware, using the CarboNIX lock and linked pusher-arm architecture with a reinforced clamp-ring interface.[1][2] The family includes 8 inch, 15 inch, 24 inch, 31.6 inch, 38.81 inch, and custom NEO diameters, with three, four, six, eight, or ten pusher springs depending on size.[1] Operating temperature is specified from -34 C to 79 C, and survival temperature is specified from -55 C to 130 C.[1] Separation velocity is tailored through discrete spring energy choices and mission-specific measurement, with average tip-off of 0.6 deg/s across axes and no axis above 2.2 deg/s for CarboNIX or NEO.[1] Payload capability is up to one ton at family level and up to 1400 kg for the 24 inch NEO configuration used on CAS500-2.[1][3][4] NEO debuted on the Bandwagon-4 mission in November 2025, and the 24 inch NEO configuration was used for the CAS500-2 deployment campaign in May 2026.[3][4] The lock mechanism is qualified to 2000 g at 1 kHz and 5000 g at 10 kHz, and the product is not subject to ITAR-type strict export regulations.[1]
- [1]NEO User Manual Revision 1.1operator datasheet2025-06-012026-05-28
- [2]Exolaunch CarboNIX NEO product pageoperator marketing-2026-05-28
- [3]Exolaunch Bandwagon-4 CarboNIX NEO debut articleoperator press2025-11-032026-05-28
- [4]Exolaunch CAS500-2 mission articleoperator press2026-05-032026-05-28