The purpose of this proposal is to develop ceramic brush shaft seals for gas turbine engines. Phase I demonstrated that ceramic brush seals can be manufactured and identified the appropriate materials. The technical objectives of this proposal are to: (1) Perfect the manufacture of an all-ceramic brush seal; (2) Test appropriate aspects of the seal; (3) Demonstrate the seal's worthiness in an engine test rig; and (4) Provide sufficient test data to fully describe the all-ceramic brush seal. Testing of the ceramic brush seals will include leakage, pressure drop, bristle wear and rotor wear for selected coatings. Bristle tufts will be used to determine wear rate, bristle load and bristle drag. These tests will be carried out over a temperature range of 80 degrees F to 1550 degrees F. Attempts will be made to determine the rotors temperature rise due to bristle rubbing. All testing will be carried out on existing rigs. A gas turbine manufacturer will be involved in all phases of the work and will test the capabilities of a ceramic brush seal in an engine rig test. It is expected that ceramic brush seals will prove to be superior to their metallic counterparts in both wear and temperature capabilities. These superior attributes of ceramic brush seals can greatly enhance the industry acknowledged performance and efficiency of brush seals