© Space Exploration Technologies Corp. All rights reserved. 70
Figure 4-14: Falcon Heavy worst-case radiated environment .............................................................. 34
Figure 4-15: Maximum spacecraft emissions .......................................................................................... 35
Figure 4-16: Fairing avionics emissions envelope ................................................................................... 36
Figure 4-17: Launch site emissions ............................................................................................................ 37
Figure 4-18: Maximum payload fairing spot temperature seen by payload ....................................... 38
Figure 5-1: On-pad electrical interfaces ..................................................................................................... 43
Figure 6-1: Space Launch Complex 40 at Cape Canaveral Space Force Station, Florida ............... 45
Figure 6-2: LC-39A at Kennedy Space Center, Florida ............................................................................ 46
Figure 6-3: Hangar AO ................................................................................................................................... 47
Figure 6-4: Layout of customer office space in Hangar AO ................................................................... 47
Figure 6-5: Space Launch Complex 4 East at Vandenberg Space Force Base, California .............. 48
Figure 6-6: Vandenberg customer office space layout ........................................................................... 49
Figure 6-7: Pad customer room .................................................................................................................. 50
Figure 6-8: Customer control rooms at SpaceX Launch Control .......................................................... 50
Figure 6-9: SpaceX’s headquarters in Hawthorne, California ................................................................ 51
Figure 6-10: SpaceX Texas test facility and test operations ................................................................. 51
Figure 7-1: Mission management organization ....................................................................................... 52
Figure 8-1: Illustrative Falcon launch vehicle processing, integration and launch operations
schedule ........................................................................................................................................................... 56
Figure 8-2: VSFB PPF and integration hangar layout .............................................................................. 57
Figure 8-3: CCSFS PPF East Bay floor plan .............................................................................................. 57
Figure 8-4: CCSFS PPF West Bay floor plan ............................................................................................. 58
Figure 8-5: Payload encapsulation and integration sequence .............................................................. 60
Figure 8-6: Integrated Falcon 9 on the transporter-erector within the integration hangar and rolling
out ..................................................................................................................................................................... 60
Figure 8-7: Launch control organization .................................................................................................... 61
Figure 8-8: SpaceX launch control at CCSFS (left) and VSFB (right) ................................................... 62
Figure 8-9: Launch vehicle rollout and erection ....................................................................................... 62
Figure 8-10: Falcon 9 sample mission profile .......................................................................................... 64
Figure 8-11: Falcon Heavy sample mission profile ................................................................................. 65
Figure 12-1: 1,575-mm interface drawing (interface plane details) ..................................................... 75
Figure 12-2: 1,575-mm interface drawing (close-out offset and keep-out volume) .......................... 76
Figure 12-3: 2,624-mm interface drawing (interface plane details) ..................................................... 77
Figure 12-4: 2,624-mm interface drawing (close-out offset and keep-out volume) .......................... 78
Figure 12-5: Payload static envelope (standard Falcon fairing) ........................................................... 79
Figure 12-6: Payload lower volume, with 1,575-mm PAF (1 of 2) ......................................................... 80
Figure 12-7: Payload lower volume, with 1,575-mm PAF (2 of 2) ......................................................... 81
Figure 12-8: Payload lower volume, with 2,624-mm PAF (1 of 2) ......................................................... 82