Rocket engine
RD-180
Rockets
Overview
A Russian two-chamber oxidizer-rich staged-combustion RP-1/LOX engine (derived from the RD-170) that powered the Atlas V first stage.
Components & hardware
Propellants
Powers
Knowledge connections
- PowersAtlas V
- Uses propellantRP-1 / LOX
Sources
The primary and reference sources this topic draws on.
- Gunter's Space PageGunter Krebs — Gunter's Space Page
A specialist reference compilation of launch vehicles, stages, and spacecraft across all spacefaring nations.