IP Library Granted Patent US 6,568,171
Granted Patent Utility
US 6,568,171 · App. 09/899,813

Rocket vehicle thrust augmentation within divergent section of nozzle

Inventor: Melvin J. Bulman
Patented Case View Patent ↗
Granted: May 27, 2003 Filed: Jul 5, 2001
Inventor
Melvin J. Bulman
Assignee (at issue)
AEROJET-GENERAL CORPORATION

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Quick Facts
Patent No.
US 6,568,171
App. No.
09/899,813
Filed
2001-07-05
Granted
2003-05-27
Kind
B2