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RD-0600

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z 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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

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