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- RD-8 abstract "The RD-8 engine was developed by Yuzhnoye Design Bureau for the second stage of the Zenit rocket. It has four hinged chambers and a single turbopump unit. The fuel pair is LOX/kerosene. Vacuum thrust is 78.5 kN and its specific impulse in vacuum is 342 seconds (3.35 km/s).The engine was designed for long service life (up to 4000 seconds), high reliability, and is the first smaller upper stage engine to use the staged combustion cycle.".
- RD-8 wikiPageID "4330864".
- RD-8 wikiPageRevisionID "603236076".
- RD-8 caption "Photo of rocket engine RD-8.".
- RD-8 countryOfOrigin Russia.
- RD-8 countryOfOrigin Soviet_Union.
- RD-8 cycle Staged_combustion.
- RD-8 fuel "rocket grade kerosene".
- RD-8 imageSize "225".
- RD-8 manufacturer Yuzhnoye_Design_Bureau.
- RD-8 name "RD-8".
- RD-8 operatingTime "1100.0".
- RD-8 oxidiser Liquid_oxygen.
- RD-8 purpose "Upper stage vernier".
- RD-8 status "Operational".
- RD-8 type "Liquid".
- RD-8 usedIn "Zenit-2, Zenit-3SL upper stage".
- RD-8 subject Category:Kerosene_rocket_engines.
- RD-8 subject Category:Rocket_engines.
- RD-8 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-8 comment "The RD-8 engine was developed by Yuzhnoye Design Bureau for the second stage of the Zenit rocket. It has four hinged chambers and a single turbopump unit. The fuel pair is LOX/kerosene. Vacuum thrust is 78.5 kN and its specific impulse in vacuum is 342 seconds (3.35 km/s).The engine was designed for long service life (up to 4000 seconds), high reliability, and is the first smaller upper stage engine to use the staged combustion cycle.".
- RD-8 label "RD-8".
- RD-8 label "RD-8".
- RD-8 label "РД-8".
- RD-8 sameAs RD-8_(mesin_roket).
- RD-8 sameAs RD-8.
- RD-8 sameAs RD-8.
- RD-8 sameAs m.0bxh_f.
- RD-8 sameAs Q5954117.
- RD-8 sameAs Q5954117.
- RD-8 wasDerivedFrom RD-8?oldid=603236076.
- RD-8 isPrimaryTopicOf RD-8.