The calculated performance of ethyl alcohol-water mixtures as rocket fuels with liquid oxygen

dc.contributor.author	A. B. P. Beeton	en_US
dc.date.accessioned	2014-10-21T15:53:01Z
dc.date.available	2014-10-21T15:53:01Z
dc.date.issued	1948	en_US
dc.identifier.other	ARC/R&M-2816	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3370
dc.description.abstract	Specific impulses and combustion temperatures have been circulated for rocket propellants consisting of liquid oxygen and ethyl alcohol-water mixtures. This system appears to have a number of advantages compared with the corresponding liquid oxygen and petrol system.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The calculated performance of ethyl alcohol-water mixtures as rocket fuels with liquid oxygen	en_US