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Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine

By Otto, Edward W.

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Book Id: WPLBN0002207795
Format Type: PDF eBook :
File Size: 14.8 MB
Reproduction Date: 2012

Title: Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine  
Author: Otto, Edward W.
Volume:
Language: English
Subject: ATMOSPHERIC TURBULENCE, FLAMMABILITY, SAFETY FACTORS
Collections: NASA Publication Collection
Historic
Publication Date:
1959
Publisher:

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A, F. R. (1959). Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine. Retrieved from http://www.ebooklibrary.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: ATMOSPHERIC TURBULENCE; FLAMMABILITY; SAFETY FACTORS; LIQUID-GAS MIXTURES; FUEL-AIR RATIO; HAZARDS; DISPERSING; DROP SIZE; DROPS (LIQUIDS); EVAPORATION; FREE FALL; JETTISONING; JP-4 JET FUEL; TURBULENT DIFFUSION

 

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