The RD-0110R (Russian: Ракетный Двигатель-0110Р (Р - рулевой), romanized: Raketnyy Dvigatel-0110R, lit. 'Rocket Engine 0110R (R - rulevoy, steering)', GRAU index: 14D24) was a rocket engine burning kerosene in liquid oxygen in a gas generator combustion cycle. It had four nozzles that can gimbal up to 45 degrees in a single axis and was used as the vernier thruster on the Soyuz-2.1v first stage.
The RD-0110R (Russian: Ракетный Двигатель-0110Р (Р - рулевой), romanized: Raketnyy Dvigatel-0110R, lit. 'Rocket Engine 0110R (R - rulevoy, steering)', GRAU index: 14D24) was a rocket engine burning kerosene in liquid oxygen in a gas generator combustion cycle. It had four nozzles that can gimbal up to 45 degrees in a single axis and was used as the vernier thruster on the Soyuz-2.1v first stage.
Source: Wikipedia "RD-0110R" · CC BY-SA 4.0
Share this article: X · Bluesky