experience.

SpaceX

Joby Aviation

8VC

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Terra Labs

USC Viterbi
Passive magnetic bearing · 3U CubeSat reaction wheel test rig
A passive magnetic bearing for a CubeSat reaction wheel, and the 40-part rig built to test it.
- 01SIZING
C360 brass flywheel sized from first principles to slew a 3U CubeSat 90° in 10 s: 0.01 N·m·s, matching Rocket Lab's flight RW-0.01.
- 02STRUCTURE
Nonmagnetic 6061 on a reconfigurable 80/20 frame, with 3D-printed fixtures. The camera tracks the rotor's orbit; a reaction torque sensor reads torque across the bearing.
- 03MODULARITY
2, 3 and 4 mm air-gap tests by single-part swap: three magnet journals share one rotor shaft, flywheel and housing.
- 04CAD + GD&T
15-parameter Siemens NX model and 11 ASME Y14.5-2018 drawings, datum frames and position tolerances matched to COTS drawings.
- 05DFM
Tooling and setup notes worked into the drawings with USC's machinist. All 11 CNC-turned and 4-axis-milled parts made first pass.
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MACH.03Terra Labs · COVE 7-DOF robotic arm 
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Designing an Automation Pipeline for High Fidelity Design Space Exploration
Custom 10N Thrust Stand.
mechanical design
custom CAD adapters for motor/load-cell and load-cell/base. table-clamped cantilevered thrust stand around a 1 kg binocular beam load cell.
- STG.01mechanical design
- STG.02electronics integration
- STG.03calibration + procedure
- STG.04characterization
- STG.05analysis






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