FALCON USER’S GUIDE 1.45 m (4.75 ft) 11.5 m (37.7 ft) 11 m (36.1 ft) 0.4 m (1.3 ft) 6.7 m (22 ft) 4.6 m (15.1 ft) PAYLOAD VOLUME (Including payload adapter) 0 m Standard 1575 mm Interface -0.91 m PAF (-3 ft) 2 Figure 5-1: Falcon fairing and payload dynamic envelope , meters (feet) The fairing can accommodate one access door in the cylindrical portion as a standard service and eight access doors as a non-standard service. The standard payload fairing door is circular, with a 24 in x 24 in size. A single through-fairing RF antenna (re-radiation) system is available as a standard service for use during payload antenna testing while on the launch pad. The service is provided for common command and telemetry frequencies. Contact SpaceX for further information on multiple re-radiation systems or non-standard frequencies. Through-fairing RF antenna (re-radiation) systems are not available for using during flight. SpaceX utilizes standard RF antennae locations on the SpaceX fairing and will work to clock the payload accordingly. Other than remove/install-before-flight items, all processing requiring access to the payload must be completed prior to fairing installation. In the event of a payload anomaly requiring customer access to the payload, the standard concept 2 Payload dynamic envelope (shown as “payload volume”) indicates the volume that the spacecraft is allowed to move within, without intrusion by the fairing due to its dynamic motions. © Space Exploration Technologies Corp. All rights reserved. 37