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-0212.html below:

RD-0212


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-0212 Part of RD-0202
RD-0212
CADB Museum, March 1992.
Credit: © Dietrich Haeseler Kosberg N2O4/UDMH rocket engine. Proton stage 3. Engine unit consisting of 1 RD-0213 main engine and 4 RD-0214 vernier/steering engines. 8D48 essentially similar to 8D411 and 8D412 and has the same combustion chamber. First flight 1967.

AKA: 8D49;RD-473. Date: 1962-68. Number: 306 . Thrust: 613.00 kN (137,807 lbf). Specific impulse: 325 s. Burn time: 230 s.

Chambers: 1 + 4.

Family: Storable liquid. Country: Russia. Launch Vehicles: Monoblock UR-500, Polyblock UR-500, Proton-K, Proton-K/D, Proton-K/DM, Proton-K/D-1, Proton-K/DM-2, Proton-K/DM-2 DM1, Proton-K/D-2, Proton-K/DM-2M, Proton-K/17S40, Proton-K/17S40 DM2. Propellants: N2O4/UDMH. Stages: Monoblock UR-500-3, Proton K-3, Proton M-3. Agency: Kosberg bureau. Bibliography: 307, 7481. Photo Gallery RD-0212
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