METHOD FOR CASTING SOLID PROPELLANT ROCKET MOTORS
Assignee
THIOKOL CORPORATION, A CORP. OF DEL.
Filed
May 24, 1983
Granted
Dec 27, 1988
Location
OGDEN UT US
Abstract
A circular slit plate having slits therein that are symmetrically positioned and originate near the center of the plate and extend radially toward the outer diameter thereof is used to deaerate solid rocket motor propellant and to provide a uniform propellant flow distribution during rocket motor casting.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Oct 17, 1983
Rescinded
Apr 4, 1988
Duration
4 years, 5 months
Inventor
- 1LARRY W. POULTER
Record Details
- Patent number
- US 4793955
- Application
- 06497538
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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