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
Angara Stage 1
RD-170
RD-170
Credit: © Mark Wade
LOx/Kerosene propellant rocket stage. Unique configuration with oxidizer in core and fuel in two tanks strapped on in parallel - all of rail-transportable 3.9 m diameter. Product of Khrunichev. Masses estimated based on engine selected and vehicle performance.

Status: Development 2004. Thrust: 8,181.13 kN (1,839,191 lbf). Gross mass: 500,000 kg (1,100,000 lb). Unfuelled mass: 40,000 kg (88,000 lb). Specific impulse: 337 s. Specific impulse sea level: 311 s. Burn time: 180 s. Height: 22.50 m (73.80 ft). Diameter: 3.90 m (12.70 ft). Span: 12.00 m (39.00 ft).



Country: Russia. Engines: RD-171. Propellants: Lox/Kerosene.

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