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Status of the Combustion Devices Injector Technology Program at the NASA MSFC
Author(s) -
Gregg Jones,
Christopher S. Protz,
Huu Trinh,
Kevin Tucker,
Tomas E. Nesman,
J. R. Hulka
Publication year - 2005
Publication title -
nasa technical reports server (nasa)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2005-4530
Subject(s) - injector , combustion , automotive engineering , aerospace engineering , aeronautics , engineering , environmental science , computer science , electrical engineering , mechanical engineering , organic chemistry , chemistry
To support the NASA Space Exploration Mission, an in-house program called Combustion Devices Injector Technology (CDIT) is being conducted at the NASA Marshall Space Flight Center (MSFC) for the fiscal year 2005. CDIT is focused on developing combustor technology and analysis tools to improve reliability and durability of upper-stage and in-space liquid propellant rocket engines. The three areas of focus include injector/chamber thermal compatibility, ignition, and combustion stability. In the compatibility and ignition areas, small-scale single- and multi-element hardware experiments will be conducted to demonstrate advanced technological concepts as well as to provide experimental data for validation of computational analysis tools. In addition, advanced analysis tools will be developed to eventually include 3-dimensional and multi- element effects and improve capability and validity to analyze heat transfer and ignition in large, multi-element injectors.

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