发明名称 |
LONG RANGE ARTILLERY SHELL |
摘要 |
A long range artillery shell (1) comprising rocket propellant mater ial (10), a rocket motor nozzle (14) and base bleed propellant material (12). Ignition of the rocket propellant material (10) is delayed until the base bleed propellant material (12) has substantially finished burning. The base bleed propellant material (12) may be housed in the same chamber and behind the rocket propellant material (10) in order to provide support to the rocket propellant material (10) during launch. The two propellant materials (10, 12) may be separated by a thermal ignition barrier (18) to prevent premature rocket ignition.
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申请公布号 |
CA2101341(A1) |
申请公布日期 |
1998.10.22 |
申请号 |
CA19932101341 |
申请日期 |
1993.07.22 |
申请人 |
THE SECRETARY OF STATE FOR DEFENCE IN HER BRITANNIC MAJESTY'S GOVERNMENT OF THE UNITED KINGDOM OF GREAT BRITAIN AND NORTHERN IRELAND;THE SECRETARY OF STATE FOR DEFENCE IN HER BRITANNIC MAJESTY'S GOVERNMENT OF THE UNITED KINGDOM OF GREAT BRITAIN AND NORTHERN IRELAND |
发明人 |
NIXON, JOHN ROBERT;LEWIN, MARTIN JAMES;SPELLWARD, TERENCE LESLIE |
分类号 |
F02K9/95;F42B10/40;(IPC1-7):F42B5/10 |
主分类号 |
F02K9/95 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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