MUSIC Flight-ready | 2nd gen qualified 2026
The most capable integrated propulsion solution for nanosatellites and microsatellites, a fully self-contained 4U system ready to integrate.
Typed specifications3 values
Discloses 2 of 10 fields engineers filter by in this category (category median 3).
- Mass
- 6 kg product page
- Propellant
- xenon product page
- Power consumption
- 100 W product page
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier11 lines, in the manufacturer's own wording
- Form factor
- 4U
- Wet mass
- 6 kg
- System power
- 100 W
- Specific impulse
- ~700 s
- Total impulse
- ~15 kNs
- Propellant
- Xe
- Satellite class
- 12U - 150 kg
- Communication interface
- Redundant CAN
- Power interface
- 25 - 36 V unregulated
- Cathodes
- 2 x MUSIC HC
- Ignition cycles
- Up to 1,600
About
The MUSIC (MUlti-Stage Ignition Compact Hall Thruster) is a flight-ready, second-generation qualified integrated propulsion solution designed for nanosatellites and microsatellites. This system is fully self-contained in a 4U form factor, including the thruster, cathodes, control electronics, and propellant tank, making it ready for integration. It has a developmental heritage, with an early version launched in 2022 aboard a 3U nanosatellite, marking the first Hall thruster flown on such a small spacecraft. In 2023, MUSIC was integrated and launched as part of a multimodal propulsion engine on a 12U satellite, enabling four-degree-of-freedom attitude and orbital control. A dual MUSIC system was delivered and environmentally qualified in 2024 for a 180 kg microsatellite platform, providing full redundancy for VLEO optical imaging operations. Future developments include a four-unit cluster for an 85 kg microsatellite to high-altitude orbit by mid-2027, targeting a total impulse of approximately 150 kNs, and a second-generation 4U COTS product operational in VLEO aboard a 16U satellite platform by 2028.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.