FIELD: chemistry.
SUBSTANCE: invention relates to rocket propellants for liquid, solid fuel and hybrid rocket engines. Rocket propellant contains fuel, which represent borazine, and oxidant. In presence of bound nitrogen in oxidant fuel additionally contains boron or its compounds, for instance, diborane, tetraborane, decaborane, beryllium borohydride, metal borides. As one of versions, rocket propellant contains as fuel 62.65±15.0% of borazine and oxidant oxygen 37.35±15.0%. As another version rocket propellant contains 34.56±13.0% of borazine, 51.52±13.0% of oxygen and 13.02±13.0% of boron. In all cases the sum of component ratios must constitute 100%.
EFFECT: invention makes it possible to obtain high energy fuel and reduce confuser of nozzle, that is, to lighten rocket engine.
4 cl
| Title | Year | Author | Number |
|---|---|---|---|
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|
RU2582712C2 |
| METHOD FOR IMPROVING PROPELLANTS AND PROPELLANT (VERSIONS) | 2014 |
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|
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|
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| STAROVEROV'S PROPELLANT - 3 (VERSIONS) | 2014 |
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| STAROVEROV'S ROCKET ENGINE 10 | 2012 |
|
RU2521429C2 |
| ROCKET PROPELLANT OR EXPLOSIVE SUBSTANCE AND METHOD OF ITS PREPARATION (VERSIONS) | 2012 |
|
RU2511370C2 |
