A RetroSearch Logo

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

Search Query:

Showing content from http://www.astronautix.com/c/../r/../r/rd-264.html below:

RD-264


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-264 Part of RD-215 Glushko N2O4/UDMH rocket engine. R-36M / RS-20A (SS-18 Mod 1) stage 1. Consists of four RD-263 engines. Used on Dnepr launch vehicle. First flight 1986.

AKA: 11D119. Date: 1969-73. Number: 42 . Thrust: 4,521.00 kN (1,016,361 lbf). Unfuelled mass: 3,600 kg (7,900 lb). Specific impulse: 318 s. Specific impulse sea level: 293 s. Height: 2.15 m (7.05 ft). Diameter: 3.03 m (9.92 ft).

Chambers: 4. Engine: 3,600 kg (7,900 lb). Chamber Pressure: 206.00 bar. Thrust to Weight Ratio: 128.05. Oxidizer to Fuel Ratio: 2.67.

Family: Storable liquid. Country: Russia. Launch Vehicles: R-36M 15A14, R-36MU 15A18, Dnepr. Propellants: N2O4/UDMH. Stages: R-36M2-1. Agency: Glushko bureau. Bibliography: 315, 323, 342, 7514. 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