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RD-184


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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-184 Glushko LOx/LCH4 rocket engine. Developed 1996-on. Attitude correction engine for apogee stage of Riksha-1 launcher project (together with RD-183). Gimbaling +/- 20 degree in two planes.

Status: Developed 1996-on. Date: 1996-. Specific impulse: 322 s. Height: 0.24 m (0.78 ft). Diameter: 0.0650 m (0.2130 ft).

In 1996 prototype development was estimated to take four years from go-ahead.

Chamber Pressure: 2.00 bar. Oxidizer to Fuel Ratio: 2.5.

Country: Russia. Launch Vehicles: Riksha. Propellants: Lox/LCH4. Agency: Glushko bureau. Bibliography: 402. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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