Km) ALLOWABLE LAUNCH AZIMUTH 25.

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 2-10.—Solid rocket motor nozzle. 2-22 135-cm (53-IN.) ACTUATOR 16.3-cm (6.4-IN.) STROKE As the water ejection, and an alarm at high oxygen.