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Development of a heat transfer test ...

Flores, Sergio.

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Development of a heat transfer test rig for finding heat transfer characteristics of liquid methane.

Record Type:	Language materials, printed : Monograph/item
Title/Author:	Development of a heat transfer test rig for finding heat transfer characteristics of liquid methane./
Author:	Flores, Sergio.
Description:	52 p.
Notes:	Source: Masters Abstracts International, Volume: 50-03, page: 1824.
Contained By:	Masters Abstracts International50-03.
Subject:	Engineering, General. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1503717
ISBN:	9781267100801

Development of a heat transfer test rig for finding heat transfer characteristics of liquid methane.
Flores, Sergio.

Development of a heat transfer test rig for finding heat transfer characteristics of liquid methane. - 52 p.

Source: Masters Abstracts International, Volume: 50-03, page: 1824.

Thesis (M.S.)--The University of Texas at El Paso, 2011.

Most large scale rocket engines use a regeneratively cooled system to cool the rocket engine using either the rocket fuel or oxidizer. The use of liquid methane as a rocket fuel is an emerging technology proving to have several advantages over current rocket fuels. However, liquid methane is lacking the extensive research as a rocket fuel compared to highly used rocket fuels like liquid hydrogen. A heat transfer test rig was built with the goal to characterize the heat transfer characteristics of liquid methane as it passes through a heated channel. The development of the test rig underwent considerations designed to replicate the conditions in a regenerative cooling channel. Experiments were first completed using liquid nitrogen in vacuum resulting in temperature data which show evidence of boiling in the channel causing vapor lock.

ISBN: 9781267100801Subjects--Topical Terms:

1020744
Engineering, General.

Development of a heat transfer test rig for finding heat transfer characteristics of liquid methane.
LDR:01757nam a2200289 4500 001 1958217
005 20140403140331.5
008 150210s2011 ||||||||||||||||| ||eng d
020 $a 9781267100801
035 $a (MiAaPQ)AAI1503717
035 $a AAI1503717
040 $a MiAaPQ $c MiAaPQ
100 1 $a Flores, Sergio. $3 2093235
245 1 0 $a Development of a heat transfer test rig for finding heat transfer characteristics of liquid methane.
300 $a 52 p.
500 $a Source: Masters Abstracts International, Volume: 50-03, page: 1824.
500 $a Adviser: Ahsan R. Choudhuri.
502 $a Thesis (M.S.)--The University of Texas at El Paso, 2011.
520 $a Most large scale rocket engines use a regeneratively cooled system to cool the rocket engine using either the rocket fuel or oxidizer. The use of liquid methane as a rocket fuel is an emerging technology proving to have several advantages over current rocket fuels. However, liquid methane is lacking the extensive research as a rocket fuel compared to highly used rocket fuels like liquid hydrogen. A heat transfer test rig was built with the goal to characterize the heat transfer characteristics of liquid methane as it passes through a heated channel. The development of the test rig underwent considerations designed to replicate the conditions in a regenerative cooling channel. Experiments were first completed using liquid nitrogen in vacuum resulting in temperature data which show evidence of boiling in the channel causing vapor lock.
590 $a School code: 0459.
650 4 $a Engineering, General. $3 1020744
650 4 $a Engineering, Mechanical. $3 783786
650 4 $a Engineering, Aerospace. $3 1018395
690 $a 0537
690 $a 0548
690 $a 0538
710 2 $a The University of Texas at El Paso. $b Civil Engineering. $3 1278205
773 0 $t Masters Abstracts International $g 50-03.
790 $a 0459
791 $a M.S.
792 $a 2011
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1503717