Electric Propulsion Gimbal Thruster Assembly
Key Features:
A MoogEP Thruster Gimbal has successfully steered the MUSES-C (Hayabusa) spacecraft to the Itokawa asteroid and returned safely to Earth. The Hayabusa II mission will have taken another journey in 2014 to Asteroid 1999 JU3.
The MoogModel-T EP Propellant Dual Axis Thruster Gimbals have successfully been used for orbit raising and station keeping of heavier payload satellites. There are multiple Model-T TGAs in flight.Ìý
- The designs are based on the MoogRotary Actuator having demonstrated a minimum of 15 year on-orbit design life on multiple missions
- ÌýHigh resolution and accuracy
- Dual axis gimbal driven by rotary actuators for crossaxis positioning
- High reliability space qualified stepper motors with Harmonic Drive transmission
- Potentiometer for position telemetry
- Two to Four propellant fuel lines with heaters/thermisters
- Available with MLI blanket
Specifications
Ìý Ìý Ìý Ìý Ìý
Large TGA | Model-T | Model-T | Model-L | Model-L |
Description | 4-Phase 70-100 VDC | 2-Phase 24 -28 VDC | 3-Phase, 1.5 deg 24 - 32 VDC | Ìý Ìý Ìý Ìý Ìý Ìý Ìý3-Phase, 1.0 deg 24 - 32 VDC Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý |
Dimension (mm)Ìý |
222 x 267 x 267 | Ìý Ìý Ìý Ìý Ìý Ìý222 x 267 x 267 Ìý Ìý Ìý | Ìý Ìý Ìý Ìý Ìý Ìý 254 x 250 x 250Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý | 254 x 250 x 250 |
Weight (Kg)Ìý | 5 | 5 | 6 | 6 |
Payload Weight Externally Supported (Kg) | 23 | 30 | 30 | 30 |
Ìý Ìý Ìý Ìý Ìý
Performance | Model-T | Model-T | Model-L | Model-L |
Total Rotational Range of Travel (deg) | +/-36 in both X & Y Axis | +/-36 in both X & Y Axis | +/-36 in both X & Y Axis | Ìý Ìý Ìý Ìý Ìý +/-36 in both X & Y AxisÌý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý |
Angular Resolution (deg) |
0.01125/step | Ìý Ìý Ìý Ìý Ìý Ìý0.01125/step Ìý Ìý Ìý | Ìý Ìý Ìý Ìý Ìý Ìý 0.0075Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý | 0.00625 |
Angular Velocity (deg/sec) | 3 | 3 | 2.25 | 1.9 |
Incremental Angular Accuracy (deg) | +/-0.003 | +/-0.003 | +/-0.003 | +/-0.003 |
Absolute Angular Accuracy (deg) | 0.03 | 0.03 | 0.015 | 0.012 |
Operating Temperature Range (deg) | -20 C to +80 C | -20 C to +100 C | -50 C to +105 C | -50 C to +105 C |
Max. Power Consumption/Actuator (Watts) | 22 | 15 | 18 | 18 |
Ìý Ìý Ìý Ìý Ìý
Medium and Small TGA | Model-M | Model-M | Model-S | Model-S |
Description | 3-Phase, 2.0 deg 24 - 32 VDC | 2-Phase, 3.0 deg 24 - 32 VDC | 3-Phase, 3.75 deg 24 - 32 VDC | Ìý Ìý Ìý Ìý Ìý Ìý Ìý2-Phase, 3.0 deg 24 - 32 VDC Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý |
Dimension (mm)Ìý |
221 x 231 x 231 | Ìý Ìý Ìý Ìý Ìý221 x 231 x 231 | Ìý Ìý Ìý Ìý Ìý Ìý 140 x 159 x 159Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý ÌýÌý | 140 x 159 x 159 |
Mount Dimensions (mm) | 100 x 100 | 100 x 100 | 76 x 76 | 76 x 76 |
Weight (Kg)Ìý | 4 | 4 | 2 | 2 |
Payload Weight Externally Supported (Kg) | 18 | 18 | 6 | 6 |
Ìý Ìý Ìý Ìý Ìý
Performance | Model-M | Model-M | Model-S | Model-S |
Total Rotational Range of Travel (deg) | +/-28 in both X & Y Axis | +/-28 in both X & Y Axis | +/-36 in both X & Y Axis | Ìý Ìý Ìý Ìý Ìý +/-36 in both X & Y AxisÌý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý |
Angular Resolution (deg) |
0.020 | Ìý Ìý Ìý Ìý Ìý Ìý0.030 Ìý Ìý | Ìý Ìý Ìý Ìý Ìý Ìý 0.0375Ìý Ìý Ìý Ìý Ìý Ìý Ìý Ìý ÌýÌý | 0.030 |
Angular Velocity (deg/sec) | 4 | 6 | 12 | 9 |
Incremental Angular Accuracy (deg) | +/-0.004 | +/-0.006 | +/-0.016 | +/-0.015 |
Absolute Angular Accuracy (deg) | 0.020 | 0.030 | 0.015 | 0.012 |
Operating Temperature Range (deg) | -50 C to +105 C | -50 C to +105 C | -50 C to +105 C | -50 C to +105 C |
Max. Power Consumption/Actuator (Watts) | 10 | 10 | 5 | 6 |
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