8D726

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

8D726

Korolev LOx/Kerosene rocket engine. GR-1 Stage 3, N-11GR - V. Development based on S1.5400.

Thrust: 66.70 kN (14,995 lbf). Specific impulse: 350 s. Burn time: 380 s.

Propellant Formulation: Lox/T-1.

Country: Russia. Launch Vehicles: GR-1, N111, N11GR. Propellants: Lox/Kerosene. Stages: N-11GR - V, GR-1 Stage 3. Agency: Korolev bureau. Bibliography: 177, 21, 64.

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