Theoretical analysis of solid propellant rockets, preparation of a solid propellant, static testing of the solid propellant in a test rocket on a test stand, determination of design parameters, and design of an 80 pound thrust rocket
dc.contributor | Graduate Program in Mechanical Engineering. | |
dc.contributor.advisor | Eraslan, Necdet, 1908- . | |
dc.contributor.author | Harput, Nurhan. | |
dc.date.accessioned | 2023-03-16T11:17:30Z | |
dc.date.available | 2023-03-16T11:17:30Z | |
dc.date.issued | 1963. | |
dc.format.extent | 30 cm. | |
dc.format.pages | 61 leaves : | |
dc.identifier.other | ME 1963 H23 | |
dc.identifier.uri | https://digitalarchive.library.bogazici.edu.tr/handle/123456789/15145 | |
dc.publisher | Thesis (M.S.) - Robert College. Faculty of Graduate School of Engineering, 1963. | |
dc.subject.lcsh | Solid propellant rockets. | |
dc.title | Theoretical analysis of solid propellant rockets, preparation of a solid propellant, static testing of the solid propellant in a test rocket on a test stand, determination of design parameters, and design of an 80 pound thrust rocket |
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