A method to measure the mass specific impulse of partially ionized helium

dc.contributor.advisorBeckmann, Herbert K.
dc.creatorPatterson, Maurice M
dc.date.accessioned2016-04-21T12:01:47Z
dc.date.available2016-04-21T12:01:47Z
dc.date.issued1960
dc.description.abstractAn apparatus to measure the mass specific impulse, Isp, of partially ionized helium flowing in a converging-diverging nozzle, was designed and fabricated. The mass specific impulse increased as the stagnation enthalpy, 110, increased. The effect on the mass specific impulse and the exit enthalpy, h2, of varying nozzle length (and area ratio) was observed. The maximum mass specific impulse measured in this investigation was approximately four times the mass specific impulse of a high performance chemical rocket fuel.
dc.format.digitalOriginreformatted digitalen_US
dc.format.extent34 ppen_US
dc.identifier.callnoThesis M.E. 1960 PATTERSONen_US
dc.identifier.citationPatterson, Maurice M. "A method to measure the mass specific impulse of partially ionized helium." (1960) Master’s Thesis, Rice University. <a href="https://hdl.handle.net/1911/89185">https://hdl.handle.net/1911/89185</a>.
dc.identifier.digitalRICE0222en_US
dc.identifier.urihttps://hdl.handle.net/1911/89185
dc.language.isoeng
dc.rightsCopyright is held by the author, unless otherwise indicated. Permission to reuse, publish, or reproduce the work beyond the bounds of fair use or other exemptions to copyright law must be obtained from the copyright holder.
dc.titleA method to measure the mass specific impulse of partially ionized helium
dc.typeThesis
dc.type.materialText
thesis.degree.departmentMechanical Engineering
thesis.degree.disciplineEngineering
thesis.degree.grantorRice University
thesis.degree.levelMasters
thesis.degree.nameMaster of Science
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