Experimental Validation of Fly-Wheel Passive Launch and On-Orbit Vibration Isolation System by Using a Superelastic SMA Mesh Washer Isolator

Table 1

Total disturbance reduction ratio, with and without isolators.

Reduction rate
Peak reduction (%)
Max.	59.32	23.65	44.37	−0.04	42.93	30.12
Mean	58.944	37.01	55.64	42.72	53.41	19.49
STD reduction (%)	52.05	22.49	58.71	15.34	42.41	32.92