FALCON USER’S GUIDE Figure 4-13: Maximum spacecraft emissions Table 4-13: Maximum spacecraft emissions Frequency Range (MHz) E Field Limit Launch Vehicle (dBμV/m) Receive System 1.0 – 1565.42 120.0 1565.42 – 1585.42 48.0 GPS L1 1585.42 – 2090.0 120.0 2090.0 – 2093.0 70.0 Stage 1 Telecommand 2093.0 – 18000.0 120.0 4.3.6.4 FAIRING EMISSIONS ENVELOPE Falcon launch vehicles have avionics inside the fairing. The fairing emission level is shown in Figure 4-14 and Table 4-14. This limit envelopes the maximum expected combined emissions from these avionics, as calculated at the surface of the payload volume in Figure 5-1. EMI safety margin is not included. © Space Exploration Technologies Corp. All rights reserved. 31