Paper Title :Higher Heat of Combustion and Exit Velocity using Butane and Liquid Oxygen in Space Shuttle
Author :Samarpan Deb Majumder
Article Citation :Samarpan Deb Majumder ,
(2017 ) " Higher Heat of Combustion and Exit Velocity using Butane and Liquid Oxygen in Space Shuttle " ,
International Journal of Advances in Mechanical and Civil Engineering (IJAMCE) ,
pp. 19-20,
Volume-4,Issue-6
Abstract : This article presents the increase in the values of the heat of combustion and the exit velocity through the nozzle
of a space shuttle using butane (fuel) and liquid oxygen (oxidiser). With the increase in the value of specific heat ratio, Me
and r (mixture ratio), we are able to achieve the same. All the calculations required have been discussed here.
Keywords - Combustion, exit velocity, fuel, butane and liquid oxygen.
Type : Research paper
Published : Volume-4,Issue-6
DOIONLINE NO - IJAMCE-IRAJ-DOIONLINE-10373
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Copyright: © Institute of Research and Journals
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Published on 2018-02-08 |
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