Evaluation and improvement of liquid propellant rocket chugging analysis techniques, final report. Part II, A study of low frequency combustion instability in rocket engine preburners using a heterogenous stirred tank reactor model [microform] / prepared by Timothy A. Bartrand.

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Bibliographic Details
Main Author:	Bartrand, Timothy A.
Corporate Author:	United States. National Aeronautics and Space Administration
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, DC] : [National Aeronautics and Space Administration], [1987]
Series:	NASA contractor report ; NASA CR-182724.
Subjects:	Rocket engines > Combustion.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:182724
NAS 1.26:182724	Restricted Place a Hold