Type 11 Biaxial Gimbal
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Specifications
Characteristic |
Units | Basis | Data |
Output Step Angle* |
Degrees | Standard | .0375 |
Steps/Revolution* | - | Standard | 9600 |
Harmonic Drive Ratio* | - | Standard | 100:1 |
Output Step Rate* | Step/Sec (Deg/Sec) | Maximum | 250 (9.375) |
Power* | Watts | Nominal | 5 |
Output Torque* | lb-in | Typical | 70 |
N-m | Typical | 8 | |
Holding Torque Powered* | lb-in | Typical | 70 |
N-m | Typical | 8 | |
Unpowered* | lb-in | Typical | 20 |
N-m | Typical | 2.26 | |
Torsional Stiffness in the AZ-EL Plane | lb-in/rad | Typical | 30,000 |
N-m/rad | Typical | 3,390 | |
Perpendicular to Plane | lb-in/rad | Typical | 15,000 |
N-m/rad | Typical | 1,695 | |
Output Flange Load Capability Axial | lb | Maximum | 350 |
N | Maximum | 1,556 | |
Transverse | lb | Maximum | 400 |
N | Maximum | 1,779 | |
Moment | lb-ft | Maximum | 540 |
N-m | Maximum | 61 | |
Total Assembly Weight | lb | Typical | 2.9 |
kg | Typical | 1.32 |
*Total Assembly Weight
Please contact Moog application engineers to discuss optional actuator performance requirements.
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