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| | Ejection |
 | | Due to differential pressure, the q-actuated selector allows activation of a 1-second TDI to the barostat lock initiator and blocks propagation to the rocket motor upper nozzle when aircraft speed is less than 300 knots. |
 | | The post ejection system consists of the barostat lock initiator, the recovery parachute catapult, the recovery parachute, a 3.0-second TDI, a 7.0-second TDI, the impact attenuation bag, the UHF antenna, the recovery parachute repositioning release retractor, and the stabilization/brake parachute cutters. |
 | | The barostat lock initiator is located on the explosive component support bracket in the rocket motor compartment. |
| f-111.net /ejection.htm (4754 words) |
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