FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, particularly to methods of intensification and control of internal ballistic characteristics of hybrid rocket engines. When increasing a hybrid rocket engine thrust, mass consumption of a solid-phase fuel component, which is polymethyl methacrylate, is changed by affecting the charged particles in flame. For this purpose, an electrostatic field is created in a combustion chamber of the hybrid rocket engine by means of a high-voltage system, including a high-voltage source and two electrodes.
EFFECT: invention increases the combustion rate of solid fuel component in the combustion chamber and increases the hybrid rocket engine thrust.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR CREATING ELECTRIC PROPULSION THRUST | 2016 |
|
RU2633075C1 |
| FUEL BURNING METHOD AND DEVICE INTENDED FOR ITS EMBODIMENT | 1996 |
|
RU2160414C2 |
| DEVICE FOR REDUCING EMISSIONS OF CARBON MONOXIDE AND NITROGEN OXIDE WHEN UTILIZING SOLID WASTE BY INCINERATION | 2020 |
|
RU2752939C1 |
| HYDROCARBON FUEL COMBUSTION METHOD AND DEVICE FOR ITS IMPLEMENTATION | 2017 |
|
RU2675732C2 |
| METHOD FOR CREATING ELECTRIC PROPULSION THRUST | 2016 |
|
RU2635951C1 |
| METHOD FOR EFFICIENT COMBUSTION OF FUEL AND DEVICE FOR ITS REALISATION | 2010 |
|
RU2448300C2 |
| IONIC ROCKET ENGINE AND METHOD OF OPERATION THEREOF | 2019 |
|
RU2738136C1 |
| IONIC ROCKET ENGINE AND METHOD OF ITS OPERATION | 2019 |
|
RU2724375C1 |
| SOLID-PROPELLANT ROCKET ENGINE | 2023 |
|
RU2821678C1 |
| METAL OR METALLOID NANOPARTICLES PLASMAJET | 2013 |
|
RU2534762C1 |
