Isayev 218

Engine · Russia

Original archive entry. The text, images and links below are kept as they were written.

Isayev Nitric acid/Amine rocket engine.

Thrust (sl): 166.000 kN (37,318 lbf). Thrust (sl): 17,000 kgf. Propellant Formulation: AK27I/TG-02.

Related