Characterisation of mechanical and thermal properties of double base propellant

Basit Öğe Kaydı
dc.contributor.authorDirikolu, M. Hüsnü
dc.contributor.authorKalaycioglu, Barış
dc.date.accessioned2020-06-25T17:49:19Z
dc.date.available2020-06-25T17:49:19Z
dc.date.issued2010
dc.departmentKırıkkale Üniversitesi
dc.description.abstractA double base propellant is a polymer which is used as an energetic material to propel rockets. Advances in computers are making it possible to simulate a rocket as a whole, i.e. structurally and thermally. Among the rocket elements, little literature exists regarding the thermal and mechanical properties of propellants at a specified environment. In this study, a double base propellant is produced and then characterised. Accordingly, tensile specimens of the propellant are prepared according to JANNAF specifications to determine its mechanical properties. The tests are carried out at a possible 74 degrees C and also at varying crosshead speeds of 1.3, 6 and 30 mm min(-1). As of the thermal properties, the heat conduction coefficient, the specific heat and the density have been determined. All these properties complete the basic data for a thermomechanical simulation of a rocket on computer.en_US
dc.identifier.citationclosedAccessen_US
dc.identifier.doi10.1179/143307510X12777574295028
dc.identifier.endpage300en_US
dc.identifier.issn1432-8917
dc.identifier.issn1433-075X
dc.identifier.issue4en_US
dc.identifier.scopus2-s2.0-77956796897
dc.identifier.scopusqualityQ2
dc.identifier.startpage297en_US
dc.identifier.urihttps://doi.org/10.1179/143307510X12777574295028
dc.identifier.urihttps://hdl.handle.net/20.500.12587/4690
dc.identifier.volume14en_US
dc.identifier.wosWOS:000282003600007
dc.identifier.wosqualityQ3
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherManey Publishingen_US
dc.relation.ispartofMaterials Research Innovations
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectMaterial testingen_US
dc.subjectDouble baseen_US
dc.subjectPropellanten_US
dc.subjectRocket simulationen_US
dc.titleCharacterisation of mechanical and thermal properties of double base propellanten_US
dc.typeArticle

Dosyalar

Orijinal paket
Listeleniyor 1 - 1 / 1
[ X ]
İsim:
Characterisation of mechanical and thermal properties of double base propellant.pdf
Boyut:
611.46 KB
Biçim:
Adobe Portable Document Format
Açıklama:
Tam Metin/Full Text
İndir

Koleksiyon

WOS İndeksli Yayınlar Koleksiyonu
Makale Koleksiyonu
Scopus İndeksli Yayınlar Koleksiyonu