"Sensitivity of rocket engine stability to propellant feed system dynamics."
Because of the increased reliability required of rocket systems in their more recently assigned missions, previously acceptable design features must be reappraised ad refined. In the region of rocket engine system stability, the probles is centered in two areas, the combustor and the propellant feed...
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University of Alabama in Huntsville Archives
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| Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/10395 |
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Electronic |
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Saturn V Collection |
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University of Alabama in Huntsville Archives |
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University of Alabama in Huntsville Archives |
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Documents |
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Documents "Sensitivity of rocket engine stability to propellant feed system dynamics." Iwanicki, L. R. |
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Documents Saturn project Rocket engines--Fuel systems Space vehicles Feed systems Combustion Stability |
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Because of the increased reliability required of rocket systems in their more recently assigned missions, previously acceptable design features must be reappraised ad refined. In the region of rocket engine system stability, the probles is centered in two areas, the combustor and the propellant feed system The principal interest of this paper lies in the coupling that occurs between the feed system and combustion dynamics, often termed a "buzzing" instability then the dymics are characterized by periodic pressure oscillations in the range of 200 to 1000 cps appearing in the combustion chamber and' the feed system. |
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"Sensitivity of rocket engine stability to propellant feed system dynamics."Iwanicki, L. R.Saturn projectRocket engines--Fuel systemsSpace vehiclesFeed systemsCombustionStabilityBecause of the increased reliability required of rocket systems in their more recently assigned missions, previously acceptable design features must be reappraised ad refined. In the region of rocket engine system stability, the probles is centered in two areas, the combustor and the propellant feed system The principal interest of this paper lies in the coupling that occurs between the feed system and combustion dynamics, often termed a "buzzing" instability then the dymics are characterized by periodic pressure oscillations in the range of 200 to 1000 cps appearing in the combustion chamber and' the feed system.1963-08-01TextDesign Reviewssensofrockengistabtopropfeedsystdyna_040607115532.pdfspc_stnv_000801http://libarchstor2.uah.edu/digitalcollections/items/show/10395http://libarchstor2.uah.edu/digitalcollections/files/original/20/10395/sensofrockengistabtopropfeedsystdyna_040607115532.pdfSaturn V CollectionBox 9, Folder 20University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabamaenspc_stnv_000800_000824This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. |
| title |
"Sensitivity of rocket engine stability to propellant feed system dynamics." |
| titleStr |
"Sensitivity of rocket engine stability to propellant feed system dynamics." |
| author |
Iwanicki, L. R. |
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Iwanicki, L. R. |
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UAHsaturnv10395 |
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http://libarchstor2.uah.edu/digitalcollections/items/show/10395 |
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1790443372741132288 |