Apogee main engine is single-chamber, single-mode, multiple firing, with propellant-pressurized feed system.
It is designed for SC add-on injection into orbits, including geostationary orbit.
BASIC SPECIFICATIONS
|
Engine mass, kg |
4.3 |
|
Propellant components: |
АТ+НДМГ |
|
Vacuum thrust, kgf |
40,7 |
|
Vacuum specific impulse, s |
315 |
|
Propellant mixture ratio |
2,05 |
|
Number of firings |
100 |
|
TRL |
6 |
back to the catalog
