FIELD: engines and pumps.
SUBSTANCE: rocket engine contains a combustion chamber where borane, or silane, or phosphene, or germane, or other hydrides with a positive enthalpy of formation from simple substances or their mix are fed. The named above substances a fed at the temperature ensuring self-sustaining course of reaction of their thermal decomposition due to heat of exothermic reaction. Another invention of the group relates to the liquid or solid fuel rocket engine into the combustion chamber of which in addition to stoichiometric composition of the main fuel borane, or silane, or phosphene, or germane, or other hydrides, or methane are fed. Another one invention of the group relates to the solid fuel rocket engine in which solid hydrides in addition to stoichiometric composition of the main fuel are a part of solid rocket fuel.
EFFECT: group of inventions allows to increase a specific impulse of a rocket engine.
9 cl
| Title | Year | Author | Number |
|---|---|---|---|
| STAROVEROV ROCKET ENGINE (VERSIONS) | 2012 |
|
RU2601820C1 |
| STAROVEROV'S PROPELLANT-6 | 2014 |
|
RU2570010C2 |
| STAROVEROV'S ROCKET ENGINE-6 (VERSIONS) | 2012 |
|
RU2570913C2 |
| STAROVEROV-4 ROCKET ENGINE /VERSIONS/ | 2012 |
|
RU2586211C2 |
| STAROVEROV'S POWDER - 2 | 2012 |
|
RU2500659C2 |
| STAROVEROV ROCKET ENGINE - 3 (VERSIONS) | 2012 |
|
RU2482313C1 |
| STAROVERV'S ROCKET ENGINE-9 (VERSIONS) | 2012 |
|
RU2570910C2 |
| STAROVERV'S ROCKET ENGINE-2 (VERSIONS) | 2012 |
|
RU2570911C2 |
| STAROVEROV'S SHOT - 5 (VERSIONS) | 2012 |
|
RU2486434C1 |
| STAROVEROV - 5 ROCKET ENGINE /VERSIONS/ | 2012 |
|
RU2586442C2 |
