POWER PLANT FOR SPACECRAFT WITH ELECTRICAL GENERATOR Russian patent published in 2008 - IPC B64G1/42 B64G1/40 

FIELD: engines and pipes.

SUBSTANCE: suggested power plant includes electrochemical generator, the rocket propulsion and connected with it schemas of keeping and feeding by hydrocarbon fuel and oxygen. To the device it is included consequently connected the reformer of partial oxidation and gas separator with output manifold of cleaned and not cleaned hydrogen. Besides, it is added the startup hydrogen bluster, connected with electrochemical generator. The output of reformer is connected to the systems of keeping and feeding by hydrocarbon fuel and oxygen. The output manifold of cleaned and not cleaned hydrogen is connected with startup hydrogen bluster and with electrochemical generator, and the input manifold of cleaned and not cleaned hydrogen is connected with the rocket propulsion. The rocket propulsion is using not cleaned hydrogen in the mix of fuel.

EFFECT: it is created adaptive for long spacecraft flights the power-propulsion plants.

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