FALCON USER’S GUIDE Figure 8-5: Payload encapsulation and integration sequence ...................................................................................................... 56 Figure 8-6: Integrated Falcon 9 on the transporter-erector within the integration hangar and rolling out .......................... 56 Figure 8-7: Launch control organization ............................................................................................................................................ 57 Figure 8-8: SpaceX launch control at CCAFS (left) and VAFB (right) ........................................................................................... 58 Figure 8-9: Launch vehicle rollout and erection ............................................................................................................................... 58 Figure 8-10: Falcon 9 sample mission profile .................................................................................................................................. 60 Figure 8-11: Falcon Heavy sample mission profile ......................................................................................................................... 61 LIST OF TABLES Table 1-1: Key safety features of Falcon launch vehicles ................................................................................................................ 3 Table 2-1: Falcon dimensions and characteristics ............................................................................................................................ 7 Table 3-1: Falcon 9 and Falcon Heavy launch services ................................................................................................................. 10 Table 4-1: Recommended quasi-static load factors for transportation ...................................................................................... 14 Table 4-2: Temperature and cleanliness environments ................................................................................................................. 14 Table 4-3: Falcon 9 maximum predicted acoustic environment (P95/50), 60% fill-factor ...................................................... 20 Table 4-4: Falcon 9 maximum predicted acoustic environment (P95/50), 60% fill-factor ...................................................... 22 Table 4-5: Falcon Heavy maximum predicted acoustic environment (P95/50), 60% fill-factor, 135.2 dB OASPL (third octave) ...................................................................................................................................................................................................... 23 Table 4-6: Falcon Heavy maximum predicted acoustic environment (P95/50), 60% fill-factor, 135.6 dB OASPL (full octave) ...................................................................................................................................................................................................... 25 Table 4-7: Payload adapter-induced shock at the spacecraft separation plane (P95/50) ...................................................... 25 Table 4-8: Falcon 9/Heavy random vibration maximum predicted environment (P95/50) at top of PAF [5.13 GRMS] .... 27 Table 4-9: Falcon 9 RF systems characteristics .............................................................................................................................. 28 Table 4-10: Falcon Heavy RF systems characteristics .................................................................................................................. 28 Table 4-11: Falcon 9 worst-case radiated environment ................................................................................................................. 29 Table 4-12: Falcon Heavy worst-case radiated environment ........................................................................................................ 30 Table 4-13: Maximum spacecraft emissions ................................................................................................................................... 31 Table 4-14: Fairing avionics emissions envelope ............................................................................................................................ 32 Table 4-15: Launch site emissions ..................................................................................................................................................... 33 Table 4-16: Spacecraft environmental compatibility verification example ................................................................................ 35 Table 5-1: Payload electrical interface connectivity ........................................................................................................................ 38 Table 5-2: Maximum expected cable lengths between payload racks/EGSE and the separation plane .............................. 39 Table 7-1: Standard launch integration schedule ............................................................................................................................ 50 Table 7-2: Required documents and data for all payloads ............................................................................................................ 51 Table 7-3: Additional required documents and data for non-US persons and non-US government payloads .................... 51 Table 8-1: Services and equipment for payload processing .......................................................................................................... 54 Table 8-2: Launch control organization ............................................................................................................................................. 57 Table 8-3: Falcon 9 sample flight timeline—GTO mission ............................................................................................................. 62 Table 8-4: Falcon 9 sample flight timeline—LEO mission .............................................................................................................. 62 LIST OF ACRONYMS ACS ..................................................................................................................................................................... attitude control system AFSPCMAN .................................................................................................................................. Air Force Space Command Manual AWG ........................................................................................................................................................................ American wire gauge © Space Exploration Technologies Corp. 66 SpaceX Proprietary and Competition-Sensitive Information.