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    • 2. 发明专利
    • Inflatable rocket-launching pad
    • GB2385112A
    • 2003-08-13
    • GB0203138
    • 2002-02-09
    • USTINOW NIKOLAI
    • USTINOW NIKOLAI
    • F41F3/04F41F7/00
    • A rocket launch pad comprises an inflatable ring-shaped body 5, and has a buoyancy force which is capable of compensating the weight of an associated payload/rocket and it's propellants. The pad additionally comprises a network of clasping ropes 6, and a plurality of first and second stage air-breathing rocket engines 2, 3 respectively, windpipes 4 and a hot water container 1. The meridian curve of the ring shaped pad is described by the equation ((dY')/(1+(Y') 2 ) 3/2 )=(kr/l)(X)(dX) where X and Y are cartesian coordinates and Kr and 1 are constant values. The inflatable body 5, preferably having a plastic foam cover, may also be filled with hydrogen gas which may also act as a fuel for the first stage air-breathing rocket engines 2. The second stage rocket engines 3 are described as being compact nuclear rockets. In additional to the general application as a rocket launch pad, the invention is also described as being applicable to unmanned lunar flights with the aim of disposing radioactive waste.