The spacecraft spin test facility is used to test and correct spacecraft balance using either dynamic or static/coupled measurement techniques to force the spin axis to the desired principle axis of the satellite and to verify the moments of inertia on large capacity moment of inertia tables.
Spacecraft Spin Test Facility
Main menu
- Division Overview
- Research Areas
- Branches
- Programs
- Facilities
- Composites Lab
- Fuels Testing Lab
- Modal Survey Test Facility
- Payload Processing Facility
- Radio Frequency Anechoic Chamber
- Radio Frequency Compact Range
- Robotics Engineering and Control Lab
- Smart Structures Research Lab
- Acoustic Reverberation Chamber
- Mechanical Inspection and Optical Alignment
- Propulsion System Welding Facility
- Spin Test Facility
- Static Test Loads Facility
- Vibration Test Facility
- RESHAPE
- Thermal Vacuum Chamber
- Two-Phase Thermal Lab