Cosmonautic Vehicles TRIZ Cases
- Hybrid Vibration Isolator with Elastomeric Hexapod Pivots
Elastomeric end pieces enable isostatic flexible pivots that resist launch stresses while active control attenuates low-frequency disturbances.
- Conical Scanning Spacecraft Sun Pointing with Cant Sensor
Canted incidence angle sensor enables conical scanning to align spacecraft axis with the Sun, reducing sensor complexity and cost.
- Solar Array Momentum Control via Selective Cell Deactivation
Selective solar cell section deactivation generates differential radiation pressure torque, unloading reaction wheel momentum without thruster fuel consumption.
- Miniature Satellite Deployable Release Mechanism Using Threaded Interface
A miniature release mechanism secures nanosatellite deployables using a threaded interface and retracting pins.