Figure 40: Z-Axis Vibration Spectrum; Table 19: Random Vibration Spectrum - Quasonix TIMTER Installation And Operation Manual

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.
90 Quasonix, Inc.

Table 19: Random Vibration Spectrum

Breakpoints
Frequency (Hz) PSD (g2/Hz)
20
30
150
200
2000
G (RMS) = 19.6

Figure 40: Z-axis Vibration Spectrum

TIMTER™ Multi-mode Dual
Telemetry Transmitter
0.04
0.17
0.17
0.2
0.2