The RD-0210 is a type of rocket engine developed for use in space exploration. It is designed to provide thrust for various spacecraft, contributing to missions that require reliable propulsion systems. The engine operates on a combination of liquid propellants, which enhances its efficiency and performance in different stages of flight. This engine is part of a broader family of engines used in the Russian space program and has been utilized in several launch vehicles. Its design focuses on maximizing thrust while minimizing weight, making it suitable for both orbital and suborbital missions.