FALCON USER’S GUIDE 11 QUICK REFERENCE LIST OF FIGURES Figure 1-1: SpaceX vehicles are designed for high cross-platform commonality ....................................................................... 2 Figure 2-1: Falcon 9 overview ................................................................................................................................................................ 5 Figure 2-2: The Falcon Heavy demonstration mission launched from KSC on February 6, 2018 ........................................... 6 Figure 2-3: Falcon Heavy first-stage engine layout ........................................................................................................................... 7 Figure 2-4: Falcon vehicle coordinate frame ...................................................................................................................................... 9 Figure 3-1: SpaceX payload attach fitting ......................................................................................................................................... 11 Figure 3-2: Allowable center-of-gravity height above the 1575-mm plane ................................................................................. 12 Figure 4-1: Falcon 9 and Falcon Heavy payload design load factors for “standard” mass (over 4,000 lb) .......................... 16 Figure 4-2: Falcon 9 payload design load factors, light mass (under 4,000 lb) ......................................................................... 17 Figure 4-3: Maximum axial equivalent sine environment for Falcon 9 and Falcon Heavy ...................................................... 18 Figure 4-4: Maximum lateral equivalent sine environment for Falcon 9 and Falcon Heavy ................................................... 19 Figure 4-5: Falcon 9 maximum predicted acoustic environment (P95/50), 60% fill-factor, 131.3 dB OASPL (Cape Canaveral) and 131.4 dB OASPL (Vandenberg) in third octave .................................................................................................... 20 Figure 4-6: Falcon 9 maximum predicted acoustic environment (P95/50), 60% fill-factor, 131.4 dB OASPL (Cape Canaveral) and 131.6 OASPL (Vandenberg) in full octave ............................................................................................................. 21 Figure 4-7: Falcon Heavy maximum predicted acoustic environment (P95/50), 60% fill-factor, 135.2 dB OASPL (third octave) ...................................................................................................................................................................................................... 23 Figure 4-8: Falcon Heavy maximum predicted acoustic environment (P95/50), 60% fill-factor, 135.6 dB OASPL (full octave) ...................................................................................................................................................................................................... 24 Figure 4-9: Falcon 9/Heavy random vibration maximum predicted environment (P95/50) at top of PAF [5.13 GRMS] .. 26 Figure 4-10: Falcon 9/Heavy frequency bin breakdown ................................................................................................................. 27 Figure 4-11: Falcon 9 worst-case radiated environment ................................................................................................................ 29 Figure 4-12: Falcon Heavy worst-case radiated environment ...................................................................................................... 30 Figure 4-13: Maximum spacecraft emissions .................................................................................................................................. 31 Figure 4-14: Fairing avionics emissions envelope ........................................................................................................................... 32 Figure 4-15: Launch site emissions .................................................................................................................................................... 33 Figure 4-16: Maximum payload fairing spot temperature seen by payload ............................................................................... 34 Figure 5-1: Falcon fairing and payload dynamic envelope, meters (feet) ................................................................................... 37 Figure 5-2: On-pad electrical interfaces ............................................................................................................................................. 39 Figure 6-1: Space Launch Complex 40 at Cape Canaveral Air Force Station, Florida .............................................................. 41 Figure 6-2: LC-39A at Kennedy Space Center, Florida .................................................................................................................... 42 Figure 6-3: Hangar AO ........................................................................................................................................................................... 43 Figure 6-4: Layout of customer office space in Hangar AO ........................................................................................................... 43 Figure 6-5: Space Launch Complex 4 East at Vandenberg Air Force Base, California ............................................................. 44 Figure 6-6: Vandenberg customer office space layout ................................................................................................................... 45 Figure 6-7: Pad customer room .......................................................................................................................................................... 46 Figure 6-8: Customer control rooms at SpaceX Launch Control.................................................................................................. 46 Figure 6-9: SpaceX’s headquarters in Hawthorne, California ........................................................................................................ 47 Figure 6-10: SpaceX Texas test facility and test operations ......................................................................................................... 47 Figure 7-1: Mission management organization ............................................................................................................................... 48 Figure 8-1: Illustrative Falcon launch vehicle processing, integration and launch operations schedule ............................. 52 Figure 8-2: VAFB payload processing facility and integration hangar layout ............................................................................ 53 Figure 8-3: CCAFS PPF East Bay floor plan ...................................................................................................................................... 53 Figure 8-4: CCAFS PPF West Bay floor plan ..................................................................................................................................... 54 © Space Exploration Technologies Corp. 65 SpaceX Proprietary and Competition-Sensitive Information.