COOLABLE ROCKET NOZZLE FOR A ROCKET ENGINE
Assignee
UNITED TECHNOLOGIES CORPORATION, A CORP. OF DE.
Filed
Feb 8, 1989
Granted
Dec 10, 1996
Location
TEQUESTA FL US
Abstract
This invention relates to rocket engines which have a rocket nozzle for expanding hot, highly pressurized rocket gases and more particularly, to a high expansion ratio nozzle for such an engine by flowing the water along a wall to provide additional cooling.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jul 14, 1989
Rescinded
May 26, 1995
Duration
5 years, 10 months
Inventor
- 1JAMES B. RANNIE
Record Details
- Patent number
- US 5582000
- Application
- 07308157
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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