TIMTER™ Multi
-mode Dual
Telemetry Transmitter
90
Quasonix, Inc.
Table 19: Random Vibration Spectrum
Breakpoints
Frequency (Hz)
PSD (g2/Hz)
20
0.04
30
0.17
150
0.17
200
0.2
2000
0.2
G (RMS) = 19.6
During flight-qualification testing, the unit under test (UUT) was shaken for 30 minutes in each axis. The results are
shown in Figure 40, Figure 41, and Figure 42.
Figure 40: Z-axis Vibration Spectrum