发明名称 Solid propellant element for pulsed plasma thruster-type electrical driving mechanism of satellite drive system, serves as monolithic helix provided with complete coils, where solid propellant includes polymer material as main component
摘要 <p>The propellant element (16) serves as a monolithic helix provided with complete coils. A solid propellant includes polymer material as main component and filling material. The filling material is electrically conducting, semi-conductive and/or non-conductive filling material such as molybdenum disulfide, aluminum oxide, silicon carbide, zinc oxide and boron nitride. The polymer material consists of fluoropolymers, polyethylene, polypropylene, polyoxymethylene, polyacetal, polyethylene terephtalate and polybutylene terephthalate and copolymers. An independent claim is also included for a method for manufacturing a solid propellant element.</p>
申请公布号 DE102008058722(A1) 申请公布日期 2010.12.23
申请号 DE20081058722 申请日期 2008.11.14
申请人 ELRINGKLINGER AG 发明人 NAWAZ, ANUSCHEH;SCHLIPF, MICHAEL;HERDRICH, GEORG;AUWETER-KURTZ, MONIKA
分类号 F02K9/10 主分类号 F02K9/10
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