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
D-2 engine
Part of D-2
Polyarniy LOx/Kerosene rocket engine. R-3. Out of Production. Competing engine for 3000 km range IRBM design to study problems of long-range rockets. Developed from April 1947 until cancellation.

AKA: D-2;R-3. Status: Out of Production. Date: 1947-51. Thrust: 1,373.00 kN (308,662 lbf). Specific impulse: 288 s. Specific impulse sea level: 240 s. Burn time: 124 s.



Country: Russia. Launch Vehicles: R-3. Propellants: Lox/Kerosene. Agency: Polyarniy. Bibliography: 194, 283.

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