RetroSearch Browse

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

Showing content from http://www.astronautix.com/c/../r/../r/rd-108-8d727.html below:

RD-108-8D727

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-108-8D727 Part of RD-107 RD-107 Credit: © Mark Wade Glushko LOx/Kerosene rocket engine. Molniya 1, Molniya 8K78M-1. OKB Glushko. Used on Molniya 8K78L, 8K78M and 11A57 Stage 1. Propellants kerosene (RG-1 or T-1) / LOx. Diameter is per chamber. First flight 1964. AKA: 8D727;8D727K;8D727K, 8D727P;8D727P;RD-108. Number: 294 . Thrust: 977.00 kN (219,638 lbf). Unfuelled mass: 1,230 kg (2,710 lb). Specific impulse: 316 s. Specific impulse sea level: 251 s. Burn time: 290 s. Height: 2.86 m (9.38 ft). Diameter: 0.75 m (2.45 ft). Chambers: 4. Engine: 1,230 kg (2,710 lb). Chamber Pressure: 53.60 bar. Thrust to Weight Ratio: 80.97. Oxidizer to Fuel Ratio: 2.39. Country: Russia. Launch Vehicles: Molniya 8K78M. Propellants: Lox/Kerosene. Stages: Molniya 8K78M-1. Agency: Glushko bureau. Photo Gallery R-7 aft end Credit: © Mark Wade 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