An investigation of the oxidizer flow passages in a dual-combustion liquid rocket engine.

An investigation of the oxidizer flow passages in a dual-combustion liquid rocket engine.

Bibliographic Details
Main Author: Kelly, Robert Joseph.
Language:en_US
Published: Monterey, California. U.S. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/12458

Internet

http://hdl.handle.net/10945/12458

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