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RD-0600
RD-0600
RD-0600
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.

Status: Developed 1970-85. Date: 1970-85. Unfuelled mass: 750 kg (1,650 lb). Height: 0.90 m (2.95 ft).

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).

Family: Laser. Country: Russia. Propellants: Gas Dynamic Laser/CO+Air+N2+C2H5OH. Agency: Kosberg bureau. Bibliography: 309, 342.
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