PROPELLANT FORMULATION AND PROCESS
Assignee
COMPOSITE MATERIALS TECHNOLOGY, INC.
Filed
Oct 23, 1989
Granted
Apr 11, 1995
Location
WAYLAND MA US
Abstract
The present invention relates to metal filaments for use as fuel additives for rocket propellants, explosives, and other pyrotechnic devices. Preferred filaments are those such as zirconium, niobium and titanium (and alloys thereof) which have very high heat of combustion.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Oct 17, 1990
Rescinded
Aug 18, 1993
Duration
2 years, 10 months
Inventor
- 1JAMES WONG
Record Details
- Patent number
- US 5404813
- Application
- 07431166
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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