ZIF-IR-189
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
Solid propellant rocket stage. . Used monolithic single motor with Nylon-S propellant. Combustion chamber pressure 30-40 kg/cm2.
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
Solid propellant rocket stage. . Used monolithic single motor with Nylon-S propellant. Combustion chamber pressure 30-40 kg/cm2.