| 发明名称 |
Ballistic modifier formulation for double base propellant |
| 摘要 |
A double base propellant modifier uses a combination of a lead component, a tin component and a copper component in physical contact to effect super-rate burning of double base propellants with defined plateau and mesa burning rate characteristics. |
| 申请公布号 |
US8864923(B1) |
申请公布日期 |
2014.10.21 |
| 申请号 |
US200611342941 |
申请日期 |
2006.01.30 |
| 申请人 |
The United States of America as represented by the Secretary of the Navy |
发明人 |
Stiles Stephen N.;McCool Paul R. |
| 分类号 |
C06B25/30;C06B23/00;C06B25/18;G01N33/22 |
主分类号 |
C06B25/30 |
| 代理机构 |
|
代理人 |
Zimmerman Fredric J. |
| 主权项 |
1. A double base propellant modifier system, comprising:
a lead component; a tin component; a copper component; and plasticized nitrocellulose fibers being combined with the lead component, the tin component and the copper component. |
| 地址 |
Washington DC US |
