HIGH PERFORMANCE SPACE MOTOR SOLID PROPELLANTS
Assignee
THIOKOL CORPORATION
Filed
Aug 2, 1990
Granted
Aug 25, 1998
Location
NEWARK DE US
Abstract
A family of high performance, space motor, solid propellants based on polyglycidyl nitrate elastomer binder, ammonium perchlorate oxidizer and beryllium or beryllium hydride fuel which do not require the presence of plasticizers. A high performance, space motor, solid propellant based on a polyglycidyl nitrate elastomer binder, ammonium perchlorate or hydroxy ammonium perchlorate and beryllium or beryllium hydride optimizes performance at low solids levels.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jan 4, 1991
Rescinded
Feb 25, 1994
Duration
3 years, 1 month
Inventor
- 1RODNEY L. WILLER
Record Details
- Patent number
- US 5798480
- Application
- 07561973
- Aerospace match
- No
- Dataset source
- 35 USC §181 SO records
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