S2.253
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/Kerosene rocket engine. R-11 (Scud B) 8A61. Thrust 8300 kgf at sea level. Fuel Kerosene T-1, chemical ignition by TG-02. First flight 1953.
Thrust (sl): 71.000 kN (15,961 lbf). Thrust (sl): 7,242 kgf. Propellant Formulation: AK20I/T-1.
Subtopics
- S2.253 derivative Isayev LOx/Kerosene rocket engine. EKR (experimental winged missile). Study 1953. Derivative of S2.253 was proposed for use in EKR Stage 1 (project for an experimental winged missile).
- S2.253A Isayev Nitric acid/Kerosene rocket engine. R-11FM. Out of Production. Used in R-11FM submarine version of Scud B. Fuel Kerosene T-1, chemical ignition by TG-02. Mixture ratio derived from tank content. 81 kN sea-level.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/Kerosene
- Agency
- Isayev bureau