COATINGS FOR SOLID PROPELLANTS
Assignee
AEROJET-GENERAL CORPORATION
Filed
Oct 27, 1988
Granted
Feb 4, 1997
Location
FAIR OAKS CA US
Abstract
This invention relates to improved polyurea coating compositions for particluate solids, and especially for fillers which are useful in solid rocket propellants. The composition is a copolymer of a primary or secondary amine and 3-nitrazapentane diisocyanate.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Feb 2, 1989
Rescinded
Jul 29, 1994
Duration
5 years, 5 months
Inventor
- 1ADOLPH E. OBERTH
Record Details
- Patent number
- US 5600088
- Application
- 07263586
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
AEROJET-GENERAL CORPORATIONMore from this assignee
ROCKET MOTOR CASE USING PLANK SECTIONS AND METHODS OF MANUFACTURING
AEROJET-GENERAL CORPORATION
ROCKET MOTOR CASE USING PLANK SECTIONS AND METHOD OF MANUFACTURE
AEROJET-GENERAL CORPORATION
SUBSTITUTED 1,4-DIPHENYLBUTADIYNES AND OLIGOMERS THEREOF AS POLYMER FLUIDIZERS AND RESINS
AEROJET-GENERAL CORPORATION
ENERGETIC AZIDOMETHYL-SUBSTITUTED 1,3-DIOXOLANES
AEROJET-GENERAL CORPORATION
PREPARATION OF 2,4,6-TRINITRO-2,4,6-TRIAZA-CYCLOHEXANONE
AEROJET-GENERAL CORPORATION
LIQUID NITRATE OXIDIZER COMPOSITIONS
AEROJET-GENERAL CORPORATION
Related by domain
GAS TURBINE ENGINE COMBUSTOR HAVING TRAPPED DUAL VORTEX CAVITY
General Electric
SOLID ROCKET PROPELLANT
GAS TURBINE ENGINE FAN (U)
General Electric
TURNING VANE ARRANGEMENT FOR IR SUPPRESSORS
SIKORSKY AIRCRAFT CORPORATION
MODULAR ROCKET BOOSTED PENETRATING WARHEAD
LOCKHEED MARTIN CORP.
INTEGRAL SOLID BOOSTER AND HYBRID THRUST SUSTAINING SYSTEM AND PROJECTILE INCORPORATING THE SAME
ENVIRONMENTAL AEROSCIENCE CORPORATION