By Jane Van Nimmen; Leonard C Bruno; Linda Neuman Ezell
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Seventy-five seconds after SRB separation, SRB apogee occurred at an altitude of approximately sixty-five kilometers. SRB impact occurred in the ocean approximately 226 kilometers downrange, to be recovered and returned for refurbishment and reuse. The primary elements of each booster were the motor (including case, propellant, igniter, and nozzle), structure, separation systems, operational flight instrumentation, recovery avionics, pyrotechnics, deceleration system, thrust vector control system, and range safety destruct system (Figure 2–13).
The exhaust nozzle in the aft segment of each motor, in conjunction with the orbiter engines, steered the Space Shuttle during the powered phase of launch. The segmentedcasing design assured maximum flexibility in fabrication and ease of transportation and handling. Each segment was shipped to the launch site on a heavy-duty rail car with a specially built cover. 96 percent). The propellant was an eleven-point star-shaped perforation in the forward motor segment and a double-truncated-cone perforation in each of the aft segments and aft closure.
Its goal was to explore the relationship between solar activity and meteorological phenomena by studying the dynamic processes that occur in the troposphere, stratosphere, and thermosphere. In April, another Scout deployed the SOOS-3, a Navy navigation satellite. In June, a third Scout carried the NOVA-II, the third in a series of improved Navy Transit navigation satellites, into space. The final Scout launch of the year deployed a fourth SOOS mission in August. In September, an Atlas E launched NOAA H, a National Weather Service meteorological satellite funded by NOAA, into Sun-synchronous orbit.