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filingDate 2019-09-29-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_20873705afad5bd069470033e3030a1c
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publicationDate 2019-12-13-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-110566368-A
titleOfInvention Rankine cycle rocket engine system
abstract The invention relates to a Rankine cycle rocket engine system, which comprises a thrust chamber (1), a condenser (5), a propellant pressurization unit, an expansion machine (4), a Rankine cycle booster pump (6) and a motor, wherein the propellant pressurization unit is connected with the thrust chamber (1) and supplies fuel, the thrust chamber (1), the expansion machine (4), the condenser (5) and the Rankine cycle booster pump (6) are connected in series to form a Rankine cycle subsystem, and the expansion machine (4) is in transmission connection with the propellant pressurization unit or is simultaneously in transmission connection with the Rankine cycle booster pump (6); the propellant booster unit and/or the Rankine cycle booster pump (6) is connected to an electric motor providing additional power. Compared with the prior art, the battery has the advantages of greatly reduced weight, simplicity, reliability, easy control and low price.
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