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Visit which he made a present of the document. ORBITER PROCESSING FACILITY Figure 6-8.—Launch Pad 39-A surface arrangement. 6-16 AS. CO E „ЖП O [o^ UA rm М po Nm ACCESS ROAD-PAD A | FUEL LINE | < APU 1 9 Y OlL COOLING | | 8.4 METERS, | (27.5 FEET) 2-34 External Tank Тесіб........................ 8-13 ELECTRONIC SYSTEMS TESTS.............. 8-14 AVIONICS INTEGRATION TESTS The Shuttle Avionics integration.