Figure 3-5: Random Vibration MPE

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14 Verification Testing or verification by analysis is REQUIRED to the electromagnetic compatibility test levels and durations defined in Table 3-15 in accordance with the environments defined in this section.
3.3.7.1

IN-FLIGHT AND PRE-FLIGHT ENVIRONMENTAL EMISSIONS
Customer must ensure that Payload materials or components sensitive to RF environments are compatible with the worst-case radiated environment shown in Figure 3-6. Launch Vehicle, including Co-Payloads, and Launch Site radiated emissions, are shown in Table 3-8 and Table 3-9 respectively. EMI margin is not included.
Figure 3-6. In-Flight & Environmental Radiated Emissions / Payload Radiated Susceptibility Limit
Table 3-8: Launch Vehicle Radiated Emissions
Frequency Range (MHz)
E-Field Limit (dBμV/m)
1.00 – 2200.0 120 2200.0 – 2300.0 140 2300.0 – 18000.0 120
Table 3-9: Launch Site Radiated Emissions
Frequency Range (MHz)
E-Field Limit (dBμV/m)
1.00 – 100 120 100 – 400 132 400 – 1200 140 1200 – 1400 148 1400 – 11000 146 11000 – 18000 120 These limits envelope the expected emissions from the Launch Vehicle, Co-Payloads, and Launch Site radar transmitters. Customer should assume 26 dB of shielding from Launch Site sources when testing and integrating the Payload in either the PPF or the Hangar Annex.

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