Solid fuel ramjet composition
US5320692A · kind A · utility
2Cited by
19References
3Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 25, 1981 |
| Grant date | Jun 14, 1994 |
| Priority date | — |
| Expiry date | Nov 25, 2001 |
Classification
- Technology area (CPC C)Chemistry; Metallurgy
- CPC primaryC06D5/00
- WIPO fieldBasic materials chemistry
- WIPO sectorChemistry
Abstract
A ramjet solid fuel composed of Hydroxyl terminated polybutadiene aluminum, agnesium, and boron carbide is described. The high volumetric heating value fuel of the present invention significantly increases the distance range of missiles.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.