公开(公告)号：US06415596B1

公开(公告)日：2002-07-09

申请号：US09744627

申请日：2001-03-15

申请人： Boris Ivanovich Katorgin ,  Felix Jurievich Chelkis ,  Igor Grigorievich Storozhenko ,  Sergei Prokopievich Chernykh ,  Oleg Efimovich Batalin ,  Evgeny Shmerovich Finkelshtein ,  Alexandr Grigorievich Liakumovich ,  Benyamin Sinaevich Strelchik ,  Vladimir Serapionovich Anufriev

发明人： Boris Ivanovich Katorgin ,  Felix Jurievich Chelkis ,  Igor Grigorievich Storozhenko ,  Sergei Prokopievich Chernykh ,  Oleg Efimovich Batalin ,  Evgeny Shmerovich Finkelshtein ,  Alexandr Grigorievich Liakumovich ,  Benyamin Sinaevich Strelchik ,  Vladimir Serapionovich Anufriev

IPC分类号： F02K972

CPC分类号： C06B47/00 ,  C06B43/00 ,  C06B47/06 ,  C10L1/04 ,  F02K9/425

摘要： The present invention pertains to the field of rocketry and more precisely to liquid-propellant rocket engines and to rocket power units. This invention essentially relates to a method for increasing the specific impulse in a liquid-propellant rocket engine by using oxygen as well as a hydrocarbon fuel consisting of dicyclobutyl (C8H14). The dicyclobutyl provides for a substantial increase in the specific impulse of the liquid-propellant rocket engine when compared with kerosene. This invention also relates to a power unit for a rocket that has tanks for liquid oxygen and for the hydrocarbon fuel. Since the fuel tank is filled with dicyclobutyl (C8H14), it is thus possible to increase the thrust, the specific impulse, as well as the in-flight operation duration of the engine, and to reduce the weight of the tanks without any substantial change in the circuits of the liquid-propellant rocket engine and of the rocket power unit.

摘要翻译： 本发明涉及火箭领域，更准确地涉及液体推进剂火箭发动机和火箭动力装置。 本发明基本上涉及通过使用氧以及由二环丁基（C 8 H 14）组成的烃燃料来增加液体推进剂火箭发动机中的比冲量的方法。 与煤油相比，二环丁基提供液体推进剂火箭发动机的比冲量的显着增加。 本发明还涉及一种具有用于液氧和烃类燃料的罐的火箭动力装置。 由于燃料箱中填充有二环丁基（C 8 H 14），因此可以增加发动机的推力，比冲量以及飞行中的运行时间，并且可以减轻油箱的重量，而没有任何实质性变化 在液体推进剂火箭发动机和火箭动力装置的回路中。