RD-0214
Sign in to saveThe RD-0214 (, GRAU index: 8D811) is a vernier thruster rocket engine burning unsymmetrical dimethylhydrazine (UDMH) fuel with dinitrogen tetroxide (N2O4) oxidizer in a gas-generator cycle. It has four nozzles that can each gimbal 45 degrees in plane to provide thrust vectoring control to the RD-0212 propulsion module of Proton rocket's third stage. It is a revised version of the RD-0207 (, GRAU index: 8D67).
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Encyclopedic overview
7 sectionsContents
- Development
- History
- Versions
- Modules
- See also
- References
- External links
The RD-0214 (, GRAU index: 8D811) is a vernier thruster rocket engine burning unsymmetrical dimethylhydrazine (UDMH) fuel with dinitrogen tetroxide (N2O4) oxidizer in a gas-generator cycle. It has four nozzles that can each gimbal 45 degrees in plane to provide thrust vectoring control to the RD-0212 propulsion module of Proton rocket's third stage. It is a revised version of the RD-0207 (, GRAU index: 8D67).
== Development ==
Excerpted from Wikipedia’s “RD-0214” article, available under the CC BY-SA 4.0 licence.