SOLID PROPELLANT WITH NON-CRYSTALLINE POLYETHER/INERT PLASTICIZER BINDER
Assignee
HERCULES INCORPORATED
Filed
Aug 25, 1989
Granted
Sep 20, 1994
Location
SALT LAKE COUNT UT US
Abstract
A solid propellant composition comprising an oxidizer, a fuel and a binder, wherein the binder comprises, based on the weight of the total propellant composition: (a) from about 3 to about 12% of a non-crystalline polyether having a molecular weight of from about 1000 to about 9,000, and (b) from about 1 to about 12% of an inert plasticizer. Propellants of this invention can be used, for example, in ground-launched interceptors, air launched tactical motors, and space boosters.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Feb 28, 1990
Rescinded
Feb 22, 1994
Duration
3 years, 12 months
Inventor
- 1JOHN R. GOLENIEWSKI
Record Details
- Patent number
- US 5348596
- Application
- 00739821
- Aerospace match
- No
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
HERCULES INCORPORATEDMore from this assignee
SOLAR THERMAL PROPULSION ENGINE
HERCULES INCORPORATED
NOVEL HIGH MODULUS PAN-BASED CARBON FIBER
HERCULES INCORPORATED
INORGANIC OXIDE RESINS FOR INTERNAL OXIDATION INHIBITION OF CARBON-CARBON COMPOSITES
HERCULES INCORPORATED
ROCKET MOTOR INSULATION AND LIKE MADE WITH THIN TACKY RIBBON
HERCULES INCORPORATED
ELASTOMERIC INSULATING MATERIALS FOR ROCKET MOTORS
HERCULES INCORPORATED
THREADED POLAR OPENINGS FOR COMPOSITE PRESSURE VESSELS
HERCULES INCORPORATED