RD-0600
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Credit: KBKhA
Kosberg laser rocket engine. Space station "Skif". Developed 1970-85. Gas dynamic laser. Working medium gaseous carbon monoxide + air + nitrogen + ethanol. Flow rate up to 100 kg/s. Tests were performed at NII TP.
Beam power up to 600 kW. A second variant for dicianatethylen + nitrogen oxide was developed and tested at GIPK.
Engine: 750 kg (1,650 lb).
Related
- Family
- Laser
- Country
- Russia
- Propellants
- Gas Dynamic Laser/CO+Air+N2+C2H5OH
- Agency
- Kosberg bureau