Zenno Astronautics Z01 Crew
Three-axis, low-dipole superconducting magnetic actuator for LEO spacecraft and space station attitude control, a solid-state alternative to CMGs.
Typed specifications9 values
Discloses 3 of 8 fields engineers filter by in this category (category median 3).
- Magnetic dipole moment
- 100 A·m² product page 300 A·m²
- Mass
- 12 000 g product page 14 500 g
- Envelope (L×W×H)
- 400 x 200 x 200 mm product page 420 x 220 x 220 mm
- Power consumption
- 45 W product page 55 W
- Radiation tolerance (TID)
- 12 krad 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 supplier14 lines, in the manufacturer's own wording
- Configuration
- Three axis, low dipole (for LEO)
- Magnetic dipole moment - config a (Am2)
- 100
- Magnetic dipole moment - config b (Am2)
- 300
- Mass - config a
- 12 kg
- Mass - config b
- 14.5 kg
- Power, continuous - config a
- 45 W
- Power, continuous - config b
- 55 W
- Outside envelope h x w x l - config a
- 400 x 200 x 200 mm
- Outside envelope h x w x l - config b
- 420 x 220 x 220 mm
- Radiation tolerance
- 12 krad
- Available torque @ 100 am2 (altitude dependent)
- 2.3-4.3 mN.m
- Max torque (LEO)
- Up to 20 Nm
- Target application
- Space station / satellite attitude actuation, 50 kg and up
- Custom configurations
- >10,000 Am2 available upon request
About
Three-axis, low-dipole superconducting magnetic actuator for LEO spacecraft and space station attitude control, a solid-state alternative to CMGs.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.