发明名称 Flying-saucer propulsion system using ion rockets - has differential power motor driven generator with rotor stabilising craft
摘要 <p>The "flying saucer' propulsion system comprises a generator, pref. driven by a differential power prime mover (3) producing electrical energy for roc rocket (5, 6). All are carried in a circular plane casing (4). The generator rotor (1) is so constructed that it stabilises the craft gyroscopically. Of the ion rockets some (6) provide propulsion thrust, others (5) prevent the casing turning with the generator rotor. Condensers (9) provide high energy discharges for defence/offence. High power searchlights may be installed between thrust rockets to permit propulsion in space by light energy. Satellite craft are carried, with a better power-weight ratio than the parent, to permit operation in gravitational fields more powerful than the earth's.</p>
申请公布号 DE2642384(A1) 申请公布日期 1978.03.23
申请号 DE19762642384 申请日期 1976.09.21
申请人 BERTRAMS,JOSEF 发明人 BERTRAMS,JOSEF
分类号 B64C39/00;(IPC1-7):64D27/24 主分类号 B64C39/00
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