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    <identifier>10.57760/sciencedb.03798</identifier>
    <datestamp>2022-10-18T21:33:43Z</datestamp>
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  <dc:date>2022-10-18</dc:date>
  <dc:title>Concept of SUb-atmospheric Radio-frequency Engine (SURE) for  near space environment</dc:title>
  <dc:identifier>doi:10.57760/sciencedb.03798</dc:identifier>
  <dc:language>en</dc:language>
  <dc:description>A concept of SUb-atmospheric Radio-frequency Engine (SURE) designed for the near-space environment is proposed. The antenna wrapping quartz tube consists of two solenoid coils with variable separation distance and is driven by radio frequency power supply (13.56 MHz&amp;ndash;1 kW). The discharge involves inductive coupling under each solenoid coil and capacitive coupling between them. This novel scheme can ionize the filling air efficiently for the entire pressure range of 32&amp;sim;5332 Pa in near space. The formed plasma density and temperature are up to 2.23&amp;times;1018 m-3 and 2.79 eV, respectively. The influences of separation distance, input power, filling pressure, and the number of solenoid turns on discharge are presented in detail. This air-breathing electric propulsion system has no plasma-facing electrode and does not require an external magnetic field and is, thereby, durable and structurally compact and light.</dc:description>
  <dc:subject>Near space; plasma thruster; RF discharge; subatmospheric</dc:subject>
  <dc:creator>Xiaogang Yuan</dc:creator>
  <dc:creator>Lei Chang</dc:creator>
  <dc:creator>Xin Yang</dc:creator>
  <dc:creator>Haishan Zhou</dc:creator>
  <dc:creator>Guangnan Luo</dc:creator>
  <dc:rights>PUBLIC</dc:rights>
  <dc:rights>https://creativecommons.org/licenses/by/4.0/</dc:rights>
  <dc:type>dataset</dc:type>
  <dc:relation>http://www.doi.org/10.1109/TPS.2020.3037794</dc:relation>
  <dc:publisher>Science Data Bank</dc:publisher>
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