FIELD: chemistry.
SUBSTANCE: invention relates to rocket fuels for liquid, hard fuel and hybrid rocket engines, as well as for extreme reciprocating and turboreactive engines. As an oxidant, fuel contains ammonium dinitramide, boron or beryllium nitrates, and nitrogen pentoxide. A peculiarity of the invention consists in application of high-energy reactions and a gas-containing oxidant. Oxidant gases serve only for formation of a reaction jet.
EFFECT: fuel is characterised by the fact that it contains only a metal (beryllium, lithium, aluminium) or boron as fuel.
9 cl, 3 ex
| Title | Year | Author | Number |
|---|---|---|---|
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|
RU2547476C2 |
| ROCKET PROPELLANT | 2012 |
|
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| STAROVEROV'S PROPELLANT - 17 (VERSIONS) | 2014 |
|
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| ROCKET PROPELLANT /VERSIONS/ | 2014 |
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| OXIDISER AND THEREOF-CONTAINING PROPELLANT | 2012 |
|
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| STAROVEROV'S PROPELLANT-20 (VERSIONS) | 2014 |
|
RU2572887C1 |
| STAROVEROV'S ROCKET ENGINE-6 (VERSIONS) | 2012 |
|
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| STAROVEROV(S EXPLOSIVE - 4 /OPTIONS/ | 2014 |
|
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| METHOD FOR IMPROVING PROPELLANTS AND PROPELLANT (VERSIONS) | 2014 |
|
RU2570022C1 |
| STAROVEROV(S-18 ROCKET PROPELLANT /VERSIONS/ | 2014 |
|
RU2576857C2 |
