A RetroSearch Logo

Home - News ( United States | United Kingdom | Italy | Germany ) - Football scores

Search Query:

Showing content from http://www.astronautix.com/c/../s/../s/soyuzst-0.html below:

Soyuz ST-0


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 Soyuz ST-0 Part of R-7 Block BVGD stage series LOx/Kerosene propellant rocket stage. Gross mass includes 1190 kg of hydrogen peroxide and 280 kg of liquid nitrogen expended during ascent but not contributing to propulsion.

Status: In production. Thrust: 1,021.10 kN (229,552 lbf). Gross mass: 44,400 kg (97,800 lb). Unfuelled mass: 3,810 kg (8,390 lb). Specific impulse: 310 s. Specific impulse sea level: 264 s. Burn time: 120 s. Height: 19.60 m (64.30 ft). Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft).

Country: Russia. Engines: RD-117. Launch Vehicles: Soyuz-FG, Soyuz-ST-B, Soyuz-2-1B, Soyuz ST / Fregat ST. 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

RetroSearch is an open source project built by @garambo | Open a GitHub Issue

Search and Browse the WWW like it's 1997 | Search results from DuckDuckGo

HTML: 3.2 | Encoding: UTF-8 | Version: 0.7.4