推进剂
口径
航空学
工程类
航空航天工程
环境科学
法律工程学
机械工程
作者
Aditya Pillai,R. R. Sanghavi,C. R. Dayanandan,M. M. Joshi,J. S. Karir
出处
期刊:Defence Science Journal
[Defence Scientific Information and Documentation Centre]
日期:2001-01-01
卷期号:51 (2): 147-153
被引量:4
摘要
'This paper presents the data obrained on dynamic firing of a cellulose acetate binder-based low vulnerability ammunition (LOV A) propellant using 120 mm fin-stabilised armour piercing discarding sabot (FSAPDS) kinetic energyammunition. An optimised propellant composition formulated ~sing fine RDX as an energetic ingredient and a mixture of cellulose acetate and nitrocellulose as binder was qualified fit for firing in a high calibre gun by its successful static evaluation for absolute ballistics using high pressure closed vessel technique. Dynamic firing of the propellant processed in heptatubular geometry was undertaken to assess the propellant charge mass. This propellant achieved higher muzzle velocity as compared to the standard NQ/M119 triple-base propellant while meeting the non-vulnerability characteristics convincingly.
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