ASTM-D6811:2002 Edition

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D6811-02 Standard Test Method for Measurement of Thermal Stability of Aviation Turbine Fuels under Turbulent Flow Conditions (HiReTS Method)^{1, 2}

Published By	Publication Date	Number of Pages
ASTM	2002

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Category: ASTM

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Description

ASTM D6811-02

Historical Standard: Standard Test Method for Measurement of Thermal Stability of Aviation Turbine Fuels under Turbulent Flow Conditions (HiReTS Method)^{1, 2}

ASTM D6811

Scope

1.1 This test method covers a laboratory thermal process, using a specified apparatus for measuring the tendencies of aviation turbine fuels to deposit insoluble materials and decomposition products, such as lacquers, within a fuel system. This test method provides a quantitative result for fuel under turbulent flow conditions in 65 or 125 min.

1.2 The values stated in SI units are to be regarded as the standard.

1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Keywords

capillary; deposits; lacquers; Reynolds number; thermal stability; turbine fuel; turbulent flow

ICS Code

ICS Number Code 75.100 (Lubricants, industrial oils and related products)

DOI: 10.1520/D6811-02

Additional information

Standard Title	D6811-02 Standard Test Method for Measurement of Thermal Stability of Aviation Turbine Fuels under Turbulent Flow Conditions (HiReTS Method)<sup>1, 2</sup>
Published Code	ASTM
Publication Date	2002