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.听
- The designs are based on the MoogRotary Actuator having demonstrated a minimum of 15 year on-orbit design life on multiple missions
- 听High 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
听 听 听 听 听
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 | 听 听 听 听 听 听 听3-Phase, 1.0 deg 24 - 32 VDC 听 听 听 听 听 听 听 听 听 听 听 听 听 听 |
Dimension (mm)听 |
222 x 267 x 267 | 听 听 听 听 听 听222 x 267 x 267 听 听 听 | 听 听 听 听 听 听 254 x 250 x 250听 听 听 听 听 听 听 听 听 听 听 听 | 254 x 250 x 250 |
Weight (Kg)听 | 5 | 5 | 6 | 6 |
Payload Weight Externally Supported (Kg) | 23 | 30 | 30 | 30 |
听 听 听 听 听
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 | 听 听 听 听 听 +/-36 in both X & Y Axis听 听 听 听 听 听 听 听 听 听 听 |
Angular Resolution (deg) |
0.01125/step | 听 听 听 听 听 听0.01125/step 听 听 听 | 听 听 听 听 听 听 0.0075听 听 听 听 听 听 听 听 听 听 | 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 |
听 听 听 听 听
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 | 听 听 听 听 听 听 听2-Phase, 3.0 deg 24 - 32 VDC 听 听 听 听 听 听 听 听 听 听 听 听 听 |
Dimension (mm)听 |
221 x 231 x 231 | 听 听 听 听 听221 x 231 x 231 | 听 听 听 听 听 听 140 x 159 x 159听 听 听 听 听 听 听 听 听 听 听听 | 140 x 159 x 159 |
Mount Dimensions (mm) | 100 x 100 | 100 x 100 | 76 x 76 | 76 x 76 |
Weight (Kg)听 | 4 | 4 | 2 | 2 |
Payload Weight Externally Supported (Kg) | 18 | 18 | 6 | 6 |
听 听 听 听 听
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 | 听 听 听 听 听 +/-36 in both X & Y Axis听 听 听 听 听 听 听 听 听 听 听 |
Angular Resolution (deg) |
0.020 | 听 听 听 听 听 听0.030 听 听 | 听 听 听 听 听 听 0.0375听 听 听 听 听 听 听 听 听听 | 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 |
Resources
Datasheets, Brochures and Catalogs
Infographics
Related Markets
Space
Mooghas designed and manufactured components and systems for satellites and launch vehicles for more than 60 years.
Spacecraft Technologies
Moogis a proven leader in components, subsystems, and systems for spacecraft of all sizes, from smallsats to GEO spacecraft. Mooghas been successfully providing spacecraft controls, inspace propulsion, and major subsystems for science, military, and commercial operations for more than 60 years.