ULTRA-ULTRAHIGH BURNING RATE COMPOSITE MODIFIED DOUBLE-BASE PROPELLANTS CONTAINING POROUS AMMONIUM PERCHLORATE
Assignee
Filed
Mar 26, 1976
Granted
Jul 31, 1990
Location
AL US
Abstract
Ultra-ultrahigh burning rate composite modified double-base propellants arebtained by use of porous ammonium perchlorate as a replacement for the ultra-ultrafine ammonium perchlorate. The porous ammonium perchlorate is used in combination with aluminum powder fuel and aluminum staples, nitroglycerin as an explosive plasticizer, triacetin as a non-explosive plasticizer, stabilizers selected from resorcinol and 2-nitrodiphenylamine and other selected additives for achieving desired processing, mechanical, ballistic, and other properties of the propellant.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Sep 10, 1982
Rescinded
Feb 15, 1990
Duration
7 years, 5 months
Inventor
- 1DAVID C. SAYLES
Record Details
- Patent number
- US 4944816
- Application
- 05671221
- Aerospace match
- No
- Dataset source
- 35 USC §181 SO records
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