Aerospace Materials and Applications 2018
DOI: 10.2514/5.9781624104893.0641.0698
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Materials for Liquid Propulsion Systems

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Cited by 4 publications
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“…They need even more resistant alloys, especially due to the high temperature load in combustion chambers. According to Halchak et al (2018), different groups of alloys are used. For the nozzle, the most heavy part of an engine, Ni-alloys like Inconel 718 (used in the Space Shuttle main engine RS-25) or Inconel 600 (Vulcain 2) are the most common alloys.…”
Section: Composition Of the Anthropogenic Materialsmentioning
confidence: 99%
“…They need even more resistant alloys, especially due to the high temperature load in combustion chambers. According to Halchak et al (2018), different groups of alloys are used. For the nozzle, the most heavy part of an engine, Ni-alloys like Inconel 718 (used in the Space Shuttle main engine RS-25) or Inconel 600 (Vulcain 2) are the most common alloys.…”
Section: Composition Of the Anthropogenic Materialsmentioning
confidence: 99%