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ASTM-D6811:2007 Edition

ASTM-D6811:2007 Edition

$40.63

D6811-02(2007)e1 Standard Test Method for Measurement of Thermal Stability of Aviation Turbine Fuels under Turbulent Flow Conditions (HiReTS Method)

Published By Publication Date Number of Pages
ASTM 2007 9
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ASTM D6811-02-e1-Reapproved2007

Withdrawn Standard: Standard Test Method for Measurement of Thermal Stability of Aviation Turbine Fuels under Turbulent Flow Conditions (HiReTS Method) (Withdrawn 2013)

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; Turbulent flow conditions; Aviation turbine fuels; HireTS method; Laboratory thermal process; Thermal stability–petroleum products

ICS Code

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

DOI: 10.1520/D6811-02R07E01

PDF Catalog

PDF Pages PDF Title
1 Scope
Referenced Documents
Terminology
Summary of Test Method
2 Significance and Use
Reagents and Materials
Sampling and Sample Containers
Preparation of Apparatus
3 Standard Operating Conditions
Calibration and Standardization
Procedure
Calculation of Result
Report
TABLE 1
4 Precision and Bias
Keywords
A1. THERMAL STABILITY APPARATUS
A1.1
A1.2
5 FIG. A1.1
FIG. A1.2
6 X1. REYNOLDS NUMBER ESTIMATION
X1.1 Introduction
X1.2 Reynolds Number
X1.3 Example Estimation
FIG. A1.3
7 X2. CORRELATION WITH OTHER PROCEDURES
X2.1
X3. REPORT FORM
X3.1
8 FIG. X3.1

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