Type 33 Biaxial Gimbal Assembly
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Key Features:
- Compact two-axis gimbal
- Can accommodate RF coax rotary Joints or waveguides
- High resolution and fine pointing
- Can accommodate launch locks, caging mechanisms and cable management systems
- Configurable in El/Az or X/Y cross axis configurations
- Actuated by space qualified Moog Type 3 actuators
Specifications
Characteristic | Units | Basis | Data |
Output Step Angle* |
Degrees | Standard | 0.009375 |
Steps/Revolution* | - | Standard | 38,400 |
Harmonic Drive Ratio* | - | Standard | 160:1 |
Output Step Rate* | Step/Sec (Deg/Sec) | Maximum | 400 (3.75) |
Power* | Watts | Nominal | 10 |
Inertial Capability* | Slug ft2 | Typical | 25 |
kg-m2 | Typical | 34 | |
Output Torque* | lb-in | Typical | 150 |
N-m | Typical | 17 | |
Holding Torque Powered* | lb-in | Typical | 300 |
N-m | Typical | 34 | |
Unpowered* | lb-in | Typical | 80 |
N-m | Typical | 9.0 | |
Torsional Stiffness in the AZ-EL Plane | lb-in/rad | Typical | 150,000 |
N-m/rad | Typical | 16,950 | |
Perpendicular to Plane | lb-in/rad | Typical | 110,00 |
N-m/rad | Typical | 12,428 | |
Output Flange Load Capability Axial | lb | Maximum | 420 |
N | Maximum | 1,868 | |
Transverse | lb | Maximum | 420 |
N | Maximum | 1,868 | |
Moment | lb-ft | Maximum | 150 |
N-m | Maximum | 203 | |
Total Assembly Weight | lb | Typical | 9.6 |
kg | Typical | 4.4 |
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Space
Moog has designed and manufactured components and systems for satellites and launch vehicles for more than 60 years.
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Moog is a proven leader in components, subsystems, and systems for spacecraft of all sizes, from smallsats to GEO spacecraft. Moog has been successfully providing spacecraft controls, inspace propulsion, and major subsystems for science, military, and commercial operations for more than 60 years.