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- Q1093826 subject Q6026128.
- Q1093826 subject Q8672104.
- Q1093826 abstract "Regenerative cooling, in the context of rocket engine design, is a configuration in which some or all of the propellant is passed through tubes, channels or in a jacket around the combustion chamber or nozzle to cool the engine. This is effective because the fuel (and sometimes the oxidizer) are good coolants. The heated propellant is then fed into a special gas generator or injected directly into the main combustion chamber for combustion there.".
- Q1093826 wikiPageWikiLink Q1139203.
- Q1093826 wikiPageWikiLink Q12438.
- Q1093826 wikiPageWikiLink Q13389141.
- Q1093826 wikiPageWikiLink Q1364934.
- Q1093826 wikiPageWikiLink Q17143051.
- Q1093826 wikiPageWikiLink Q17183363.
- Q1093826 wikiPageWikiLink Q174640.
- Q1093826 wikiPageWikiLink Q182546.
- Q1093826 wikiPageWikiLink Q193701.
- Q1093826 wikiPageWikiLink Q1970020.
- Q1093826 wikiPageWikiLink Q229367.
- Q1093826 wikiPageWikiLink Q277579.
- Q1093826 wikiPageWikiLink Q2997395.
- Q1093826 wikiPageWikiLink Q31863.
- Q1093826 wikiPageWikiLink Q327279.
- Q1093826 wikiPageWikiLink Q335225.
- Q1093826 wikiPageWikiLink Q3421537.
- Q1093826 wikiPageWikiLink Q342397.
- Q1093826 wikiPageWikiLink Q400515.
- Q1093826 wikiPageWikiLink Q41239.
- Q1093826 wikiPageWikiLink Q41291.
- Q1093826 wikiPageWikiLink Q487005.
- Q1093826 wikiPageWikiLink Q5199275.
- Q1093826 wikiPageWikiLink Q6026128.
- Q1093826 wikiPageWikiLink Q62377.
- Q1093826 wikiPageWikiLink Q634340.
- Q1093826 wikiPageWikiLink Q752193.
- Q1093826 wikiPageWikiLink Q77440.
- Q1093826 wikiPageWikiLink Q78750.
- Q1093826 wikiPageWikiLink Q8672104.
- Q1093826 wikiPageWikiLink Q909434.
- Q1093826 wikiPageWikiLink Q9291410.
- Q1093826 wikiPageWikiLink Q936812.
- Q1093826 wikiPageWikiLink Q968432.
- Q1093826 comment "Regenerative cooling, in the context of rocket engine design, is a configuration in which some or all of the propellant is passed through tubes, channels or in a jacket around the combustion chamber or nozzle to cool the engine. This is effective because the fuel (and sometimes the oxidizer) are good coolants. The heated propellant is then fed into a special gas generator or injected directly into the main combustion chamber for combustion there.".
- Q1093826 label "Regenerative cooling (rocket)".