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.
Technical specifications
- Configuration
- Three axis, low dipole (for LEO)
- Magnetic dipole moment - Config A (Am2)
- 100
- Magnetic dipole moment - Config B (Am2)
- 300
- Mass - Config A (kg)
- 12
- Mass - Config B (kg)
- 14.5
- Power, continuous - Config A (W)
- 45
- Power, continuous - Config B (W)
- 55
- Outside envelope H x W x L - Config A (mm)
- 400 x 200 x 200
- Outside envelope H x W x L - Config B (mm)
- 420 x 220 x 220
- Radiation tolerance (RAD)
- 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.