发明名称 AIR-JET ROCKET ENGINE
摘要 FIELD: aviation; manufacture of space vehicles. SUBSTANCE: air-jet rocket engine has front cone and rear truncated cone which are rigidly interconnected and are revolving in radial thrust bearings fitted in intermediate middle section. Front cone is provided with screw blades which may enter its body. Air-jet rocket operated in air as follows: when counter-flow gets on screw blades of front cone, both front cone and rear truncated cone rigidly connected with it are set in rotation; working medium (water) enters dynamic nozzle of rear cone; during rotation, centrifugal force acting on blades and walls of dynamic nozzle is increased, thus creating propulsive force. Engine has high performance. Engine is simple in construction, safe and effective in operation. It may be used for space vehicles flying at speeds higher than 20.000 km/h at altitudes up to 100 km. EFFECT: enhanced efficiency. 3 dwg
申请公布号 RU94020125(A) 申请公布日期 1996.06.27
申请号 RU19940020125 申请日期 1994.05.31
申请人 TOVARISHCHESTVO S OGRANICHENNOJ OTVETSTVENNOST'JU"MERIGEL'" 发明人 ENOV M.I.
分类号 F02K9/00 主分类号 F02K9/00
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