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Influenced by the special physical characteristics of the plasma sheath and the parameters of the aircraft&#x2019;s attitude, the channel containing the plasma sheath can be regarded as a special kind of discontinuous channel. A code-division space-time fountain code form is proposed that is suitable for the spatial characteristics of the plasma sheath channel. Simulation results show that the use of code-division space-time fountain code maximizes the use of the airspace resources in the plasma sheath channel. The scheme proposed in this paper can be used to alleviate the &#x201C;ionization blackout&#x201D; problem faced by hypersonic vehicles in the reentry process.

Code-division space-time fountain code for plasma sheath communication