D-1 engine
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg isopropyl nitrate monopropellant rocket engine. Developed 1955-56. Second thrust level at 50%. Explosion of D-1 on test bench in 1956 forced stop of work with mono-propellant OT-152. Sea level thrust 39 kN.
Chamber Pressure: 35.30 bar. Propellant Formulation: OT-152.
Related
- Family
- Monopropellant
- Country
- Russia
- Propellants
- Isopropylnitrate
- Agency
- Kosberg bureau
- Bibliography
- 309