FALCON USER’S GUIDE as part of the second stage. The payload harnesses are routed along the exterior of the second-stage propellant tanks, underneath raceway covers that provide protection during ground and flight operations. At the top of the second-stage the harnesses are routed through the payload attach fitting (Section 5.1.1) and to the spacecraft separation plane. The total cable lengths between the payload racks/EGSE and the spacecraft separation plane are listed in Table 5-2 and shown in Figure 5-2. Table 5-2: Maximum expected cable lengths between payload racks/EGSE and the separation plane Launch Site PPF Hangar Launch Pad VAFB (SLC-4) 30.5 m (100 ft) 208.5 m (684 ft) 171.9 m (564 ft) CCAFS (SLC-40) 18.3 m (60 ft) 197.8 m (649 ft) 171.9 m (564 ft) KSC (LC-39A) 18.3 m (60 ft) 181.1 m (594 ft) 196.3 m (644 ft) Figure 5-2: On-pad electrical interfaces © Space Exploration Technologies Corp. All rights reserved. 39