RetroSearch Browse

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

Showing content from http://www.astronautix.com/c/../s/../r/../r/rd-0155.html below:

RD-0155

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 RD-0155 RD-0155 Credit: KBKhA Kosberg LOx/Kerosene rocket engine. Engine proposed to replace RD-107 in Onega and Avrora versions of the Soyuz launch vehicle. Status: Design concept 2007. Date: 1998-. Thrust: 902.50 kN (202,890 lbf). Specific impulse: 296 s. Specific impulse sea level: 296 s. The engine consists of two chambers, a fixed inner chamber and a gimbaled outer chamber. Chamber pressure in the fixed chamber, 180 kg/m2; in the gimbaled chamber, 160 kg/m2. Chambers: 2. Thrust (sl): 902.500 kN (202,890 lbf). Thrust (sl): 92,000 kgf. Engine: 1,150 kg (2,530 lb). Chamber Pressure: 176.00 bar. Country: Russia. Propellants: Lox/Kerosene. Agency: Kosberg bureau. Bibliography: 4484. 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