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RD-192.3


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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-192.3 Part of RD-170 Glushko LOx/LCH4 rocket engine. Developed 1996-on. Proposed variant of RD-192. Gas generator cycle. Gimbaling +/- 8 degree in two planes. Status 1998 was project based on RD-191 prototype, development estimated for four years.

Status: Developed 1996-on. Date: 1996-. Thrust: 2,089.00 kN (469,625 lbf). Specific impulse: 341 s. Specific impulse sea level: 311 s. Height: 3.62 m (11.87 ft). Diameter: 1.45 m (4.75 ft).

Chamber Pressure: 245.00 bar. Oxidizer to Fuel Ratio: 3.

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