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-0107.html below:

RD-0107


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-0107 Part of RD-0106
RD-0110 Engine
Soyuz 11A511 Stage 2 engine displayed at Tsiolkovskiy Museum in Kaluga.
Credit: © Mark Wade Kosberg LOx/Kerosene rocket engine. R-9, Molniya 8K78, Voskhod 11A57 stage 3. Out of Production. Gas generator cycle.

AKA: 8D715K;RD-461;RD-461, RO-9;RO-9. Status: Out of Production. Date: 1958-62. Thrust: 297.90 kN (66,971 lbf). Unfuelled mass: 410 kg (900 lb). Specific impulse: 326 s. Burn time: 250 s. Diameter: 0.64 m (2.09 ft).

Chambers: 4. Engine: 410 kg (900 lb). Chamber Pressure: 68.20 bar. Propellant Formulation: Lox/T-1. Thrust to Weight Ratio: 74.09.

Country: Russia. Propellants: Lox/Kerosene. Stages: Molniya 8K78-2. Agency: Kosberg bureau. Bibliography: 177, 7464. Photo Gallery RD-0107
Credit: KBKhA 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