Experimental Behavior of Pentaborane-Air Combustion Products During Expansion in a Convergent Divergent Nozzle Metadata
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Title
- Main Title Experimental Behavior of Pentaborane-Air Combustion Products During Expansion in a Convergent Divergent Nozzle
- Series Title NACA Research Memorandums
Creator
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Author: Branstetter, J. RobertCreator Type: Personal
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Author: Setze, Paul C.Creator Type: Personal
Contributor
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Originator: Lewis Flight Propulsion LaboratoryContributor Type: OrganizationContributor Info: NASA Lewis Research Center
Date
- Creation: 1958-02-18
Language
- English
Description
- Content Description: "In order to evaluate the post combustion behavior of boric oxide, pentaborane-air mixtures, burned to completion at a combustor pressure of 3 atmospheres, were expanded through a 7.1-inch-long convergent-divergent nozzle having a 4-inch-diameter throat and an exit-to-throat area ratio of 1.68. The experimentally determined thrust performance was in good agreement with the ideal equilibrium performance at stagnation temperatures of 3300 deg R and lower. The boric oxide vapor at the combustor exit required about 400 degrees F supercooling before any condensed phase was observed" (p. 1).
- Physical Description: 69 p. : ill.
Subject
- Keyword: pentaborane-air combustion
- Keyword: aircraft nozzles
Collection
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Name: National Advisory Committee for Aeronautics CollectionCode: NACA
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Name: Technical Report Archive and Image LibraryCode: TRAIL
Institution
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Name: UNT Libraries Government Documents DepartmentCode: UNTGD
Rights
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
Resource Type
- Report
Format
- Text
Identifier
- Accession or Local Control No: 67N31730
- URL: http://hdl.handle.net/2060/19670022401
- Report No.: NACA-RM-E57I20
- Center for AeroSpace Information Number: 19670022401
- Archival Resource Key: ark:/67531/metadc53119