FIELD: astronautics.
SUBSTANCE: spacecraft engine (10) containing a chemical thruster having nozzle (30) for ejecting a combustion gas, together with a Hall-effect thruster. Said engine is configured in such a way that the nozzle serves as an ejection channel for particles ejected by the Hall-effect thruster when it is running.
EFFECT: engine can provide high thrust with a low specific impulse or relatively low thrust with a high specific impulse.
12 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ENGINE ON HALL EFFECT AND SPACE VEHICLE, INCLUDING SUCH ENGINE | 2016 |
|
RU2703870C2 |
| IONIC ROCKET ENGINE OF SPACECRAFT | 2018 |
|
RU2682962C1 |
| MEMBRANE SPACECRAFT ION-PLASMA ROCKET ENGINE | 2018 |
|
RU2709231C1 |
| ENGINE ON THE HALL EFFECT | 2012 |
|
RU2620880C2 |
| PLASMA JET ENGINE BASED ON HALL EFFECT | 2010 |
|
RU2527267C2 |
| PLASMA-ROCKET ENGINE | 2019 |
|
RU2733076C1 |
| RAMJET RELATIVISTIC ENGINE | 2020 |
|
RU2776324C1 |
| PLASMA-JET ENGINE WITH GALVANOMAGNETIC HALL EFFECT | 2003 |
|
RU2319040C2 |
| SPACECRAFT LOW-THRUST ENGINE | 2004 |
|
RU2330181C2 |
| ENGINE ON THE HALL EFFECT | 2013 |
|
RU2619389C2 |
