Quasonix TIMTER Installation And Operation Manual page 104

During flight-qualification testing, the unit under test (UUT) was shaken for 30 minutes in each axis. The results are
shown in Figure 38, Figure 39, and Figure 40.
96 Quasonix, Inc.
Table 19: Random Vibration Spectrum
Breakpoints
Frequency (Hz) PSD (g2/Hz)
20
30
150
200
2000
G (RMS) = 19.6
Figure 38: Z-axis Vibration Spectrum
TIMTER™ Multi-mode Dual
Telemetry Transmitter
0.04
0.17
0.17
0.2
0.2