For sealing a turbojet shaft under extreme temperatures and pressures, options are limited primarily to labby and carbon seals. High surface velocities complicate the sealing process, leading to concerns over leakage rates with labby seals and temperature limitations for carbon face seals. Moving the seal away from the hot area or extending the shaft could be potential solutions. The discussion highlights the challenge of finding suitable high-temperature seals, as many suppliers do not cater to the specific needs of high-pressure turbine applications. Innovative cooling schemes, such as routing high-pressure bleed air, may offer some relief in managing seal performance.