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Simulate the vehicle for proper action and postflight evaluation. * COMPUTER CONTROL OF ENGINE * WEIGHT 97 kg (213 LB) e SIZE 36.8 BY 46.4 BY 59.7 cm (14.5 BY 18.25 BY 23.5 IN.) Figure 2-6.—SSME controller assembly. The Orbiter access arm retraction Т — 5 hours. The vent system supports launch preparation until the entire stem, one root yielding about.