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RD-191M


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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-191M Part of RD-170 Glushko LOx/Kerosene rocket engine. Angara stage I. Developed 1996-. Single chamber version of the RD-170 / RD-171.

Status: Developed 1996-. Date: 1996-. Thrust: 1,976.00 kN (444,222 lbf). Specific impulse: 338 s.

Propellant Formulation: Lox/RG-1.

Country: Russia. Propellants: Lox/Kerosene. 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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