S2.253 derivative
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
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).
Related
- Country
- Russia
- Launch Vehicles
- EKR
- Propellants
- Lox/Kerosene
- Stages
- EKR Stage 1
- Agency
- Isayev bureau