| 发明名称 |
Solid fuel ramjet composition |
| 摘要 |
A ramjet solid fuel composed of Hydroxyl terminated polybutadiene aluminum, magnesium, and boron carbide is described. The high volumetric heating value fuel of the present invention significantly increases the distance range of missiles.
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| 申请公布号 |
US5320692(A) |
申请公布日期 |
1994.06.14 |
| 申请号 |
US19810329621 |
申请日期 |
1981.11.25 |
| 申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY |
发明人 |
BURDETTE, GEORGE W.;MEYERS, GARY W. |
| 分类号 |
C06B45/10;C06D5/00;(IPC1-7):C06B45/10 |
主分类号 |
C06B45/10 |
| 代理机构 |
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