Development study on precooler for atrex engine

Kenya Harada; Hiroshi Yamauchi; Nobuhiro Tanatsugu; Tetsuya Sato; Yoriji Okabe; Kenji Hamabe; Junichiro Tomike; Masahide Kazari

Development study on precooler for atrex engine

Kenya Harada, Hiroshi Yamauchi, Nobuhiro Tanatsugu, Tetsuya Sato, Yoriji Okabe, Kenji Hamabe, Junichiro Tomike, Masahide Kazari

Research output: Contribution to journal › Article › peer-review

2 Citations (Scopus)

Abstract

Two types of precooler were manufactured to be integrated into ATREX engine and tested under the sea level static condition. In this report, the test results for the thermal and hydraulic characteristics of these precoolers are shown and compared with analytical predictions. The problem of non-uniformity of the air flow in the precooler was examined by numerical calculation.

Original language	English
Pages (from-to)	251-257
Number of pages	7
Journal	Advances in the Astronautical Sciences
Volume	96
Publication status	Published - 1997 Dec 1
Externally published	Yes

ASJC Scopus subject areas

Aerospace Engineering
Space and Planetary Science

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title = "Development study on precooler for atrex engine",

abstract = "Two types of precooler were manufactured to be integrated into ATREX engine and tested under the sea level static condition. In this report, the test results for the thermal and hydraulic characteristics of these precoolers are shown and compared with analytical predictions. The problem of non-uniformity of the air flow in the precooler was examined by numerical calculation.",

author = "Kenya Harada and Hiroshi Yamauchi and Nobuhiro Tanatsugu and Tetsuya Sato and Yoriji Okabe and Kenji Hamabe and Junichiro Tomike and Masahide Kazari",

year = "1997",

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language = "English",

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journal = "Advances in the Astronautical Sciences",

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AU - Harada, Kenya

AU - Yamauchi, Hiroshi

AU - Tanatsugu, Nobuhiro

AU - Sato, Tetsuya

AU - Okabe, Yoriji

AU - Hamabe, Kenji

AU - Tomike, Junichiro

AU - Kazari, Masahide

PY - 1997/12/1

Y1 - 1997/12/1

N2 - Two types of precooler were manufactured to be integrated into ATREX engine and tested under the sea level static condition. In this report, the test results for the thermal and hydraulic characteristics of these precoolers are shown and compared with analytical predictions. The problem of non-uniformity of the air flow in the precooler was examined by numerical calculation.

AB - Two types of precooler were manufactured to be integrated into ATREX engine and tested under the sea level static condition. In this report, the test results for the thermal and hydraulic characteristics of these precoolers are shown and compared with analytical predictions. The problem of non-uniformity of the air flow in the precooler was examined by numerical calculation.

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JO - Advances in the Astronautical Sciences

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