Combustion of RS-41
dc.contributor | Moxnes, John F. | en_GB |
dc.contributor | Nevstad, Gunnar Ove | en_GB |
dc.contributor | Eriksen, Svein W. | en_GB |
dc.date.accessioned | 2018-10-22T12:45:12Z | |
dc.date.available | 2018-10-22T12:45:12Z | |
dc.date.issued | 2000 | |
dc.identifier | 778 | |
dc.identifier.other | 2000/02758 | |
dc.identifier.uri | http://hdl.handle.net/20.500.12242/1648 | |
dc.description.abstract | The pyrotechnic composition RS-41, a mixture of 49 wt.% KClO4, 49 wt.% Al/Mg and 2 wt.% Calcium Resinate, is an important ingredient in the MP (Multipurpose) ammunition. RS-41 placed in the front of the projectile ignites due to impulse transfer by impact. A pyrotechnically combustion starts and spreads backward in the projectile and towards the explosive. This gives a delay that is important for the fragmentation effect of the warhead. This report do analyses Closed Vessel experiments performed on RS-41. | en_GB |
dc.language.iso | en | en_GB |
dc.title | Combustion of RS-41 | en_GB |
dc.subject.keyword | Pyroteknikk | en_GB |
dc.subject.keyword | Forbrenning | en_GB |
dc.subject.keyword | Oksidasjon | en_GB |
dc.source.issue | 2000/02758 | en_GB |
dc.source.pagenumber | 25 | en_GB |