The propellant mixture in each SRB motor consists of an ammonium perchlorate (oxidizer,
69.6 percent by weight), aluminum (fuel, 16 percent), iron oxide (a catalyst, 0.4 percent), a
polymer (a binder that holds the mixture together, 12.04 percent), and an epoxy curing
agent (1.96 percent). The propellant is an 11-point star-shaped perforation in the forward
motor segment and a double-truncated-cone perforation in each of the aft segments and aft
closure. This configuration provides high thrust at ignition and then reduces the thrust by
approximately a third 50 seconds after lift-off to prevent overstressing the vehicle during
maximum dynamic pressure.
69.6 percent by weight), aluminum (fuel, 16 percent), iron oxide (a catalyst, 0.4 percent), a
polymer (a binder that holds the mixture together, 12.04 percent), and an epoxy curing
agent (1.96 percent). The propellant is an 11-point star-shaped perforation in the forward
motor segment and a double-truncated-cone perforation in each of the aft segments and aft
closure. This configuration provides high thrust at ignition and then reduces the thrust by
approximately a third 50 seconds after lift-off to prevent overstressing the vehicle during
maximum dynamic pressure.
Joel
Comment