دانلود استاندارد GRTCA DO-160 خرید استاندارد Environmental Conditions and Test Procedures for Airborne Equipment
خرید استاندارد RTCA DO-160G
برای دانلود استاندارد RTCA DO-160G و خرید استاندارد Environmental Conditions and Test Procedures for Airborne Equipment سال 2014 و 542 صفحه بر روی کلید خرید در انتهای صفحه کلیک کنید. پس از اتصال به درگاه پرداخت و تکمیل مراحل خرید، لینک دانلود ایمیل می شود. این استاندارد در فرمت PDF ارسال می شود. توجه کنید که نسخه استاندارد 2014 می باشد.
در صورتی که نیاز به دانلود هر استانداردی از IHS و یا techstreet دارید، فقط کافیست ادرس اینترنتی استاندارد را از سایت http://techstreet.com و یا https://global.ihs.com برای ما ارسال کنید (راههای ارتباطی در صفحه تماس با گیگاپیپر ). پس از بررسی، هزینه ان اعلام می شود. پس از واریز نسخه الکترونیکی ارسال می شود.
RTCA DO-160G
Environmental Conditions and Test Procedures for Airborne Equipment
STANDARD by Radio Technical Commission for Aeronautics, 2014
For Download Please Contact Us :
Price : 50$
دانلود رایگان استاندارد RTCA DO-160 سال 2000
برای اطمینان از کیفیت استاندارد RTCA DO 160، چند صفحه ابتدایی ان بصورت رایگان قرار داده شده است.
RTCA, Inc.
1828 L Street, NW Suite 805
Washington, DC 20036
RTCA/DO-160G
Environmental Conditions and Test
Procedures for Airborne Equipment
Section 1
Purpose and Applicability
Section 2
Definitions of Terms
Section 3
Conditions of Tests
درباره استاندارد RTCA DO-160G
Published: 2014
Number of Pages:542
فهرست مطالب استاندارد RTCA DO-160 سال 2014
Table of Contents ………………………………………………………………………………………………………………………. iii
Section 1.0
Purpose and Applicability
Section 2.0
Definitions of Terms – General
Section 3.0
Conditions of Tests
Section 4.0
Temperature and Altitude
Section 5.0
Temperature Variation
Section 6.0
Humidity
Section 7.0
Operational Shocks and Crash Safety
Section 8.0
Vibration
Section 9.0
Explosion Proofness
Section 10.0
Waterproofness
Section 11.0
Fluids Susceptibility
Section 12.0
Sand and Dust
Section 13.0
Fungus Resistance
Section 14.0
Salt Spray
Section 15.0
Magnetic Effect
Section 16.0
Power Input
Section 17.0
Voltage Spike
Section 18.0
Audio Frequency Conducted Susceptibility – Power Inputs
Section 19.0
Induced Signal Susceptibility
Section 20.0
Radio Frequency Susceptibility (Radiated and Conducted)
Section 21.0
Emission of Radio Frequency Energy
Section 22.0
Lightning Induced Transient Susceptibility
Section 23.0
Lightning Direct Effects
Section 24.0
Icing
Section 25.0
Electrostatic Discharge
Section 26.0
Fire, Flammability
Appendix A
Environmental Test Identification
Appendix B
Membership
Appendix C
Change Coordinators
Note:
Detailed Tables of Contents appear on the inside of most sections.
توضیحات شرایط محیطی و رویه‌های آزمایش تجهیزات هوابرد (همچنین به ضمیمه RTCA DO-357 برای RTCA DO-160G مراجعه کنید)
Purpose and Applicability
This document defines a series of minimum standard environmental test conditions
(categories) and applicable test procedures for airborne equipment. The purpose of these
tests is to provide a laboratory means of determining the performance characteristics of
airborne equipment in environmental conditions representative of those which may be
encountered in airborne operation of the equipment.
The standard environmental test conditions and test procedures contained herein may be
used in conjunction with applicable equipment performance standards as a minimum
specification under environmental conditions, which can ensure a sufficient degree of
confidence in performance during operations.
Note:
In each of the test procedures contained herein, the following phrase will
be seen several times:
DETERMINE COMPLIANCE WITH APPLICABLE EQUIPMENT
PERFORMANCE STANDARDS.
The “applicable equipment performance standards” referred to are either:
a.
EUROCAE Minimum Operational Performance Specifications
(formerly Requirements) (MOPS/MOPR).
b.
RTCA Minimum Performance Standards (MPS) and/or RTCA
Minimum Operational Performance Standards (MOPS).
c.
The manufacturers equipment specification(s), where applicable.
Some of the environmental conditions and test procedures contained in this document are
not necessarily applicable to all airborne equipment. The selection of the appropriate
and/or additional environmental conditions and test procedures is the responsibility of the
writers (authors) of the performance standards for the specific airborne equipment.
Notes:
1.
There are several additional environmental conditions (categories), that specific
airborne equipment may need to be evaluated against, that have not been included
in this document. These include, but are not limited to: hail, acceleration and
acoustic vibration.
2.
The procedures for testing airborne equipment for special environmental
conditions that are usually uniquely related to that specific type of airborne
equipment, should be the responsibility of the writer (author) of the performance
standard for that specific equipment.
Copyright RTCA, Inc.
Provided by IHS under license with RTCA, Inc.
Licensee=BAE Birtley, Glascoed/5932949024, User=sam, albett
Not for Resale, 03/21/2016 06:55:50 MDT
No reproduction or networking permitted without license from IHS
–“,`,“,`,“,“,,,`,,,,`,`,,`,-`-`,,`,,`,`,,`—
info@GigaPaper.ir
1-2
© 2010 RTCA, Inc.
3.
The International System of Units (SI) is usually used throughout this document
as the primary values. In certain instances, however, when the primary values
were derived in US units, these units are used as the primary values.
4.
Subject to the provisions of Subsection 3.2, it is permissible to use more than one
test article.
The words airborne equipment, as used within this document, have direct applicability to
most airborne equipment. It is the responsibility of those who wish to apply the test
conditions and procedures contained in this document to determine the applicability of
these test conditions and procedures to a specific equipment intended for installation on,
or within, a specific or general class or type of aircraft.
Minimum operational performance standards (MOPS) prepared by RTCA, Inc. for
airborne equipment contain requirements that the equipment must meet to ensure reliable
operation in actual aeronautical installations. These equipment requirements must be
verified in ambient and stressed environmental conditions. The MOPS typically contain
recommended bench test procedures for ambient conditions, and refer to RTCA Document
DO-160, “Environmental Conditions and Test Procedures for Airborne Equipment,” for
the stressed environmental testing. The test categories defined in DO-160 are intended to
encompass the full spectrum of environmental conditions that airborne equipment may
experience – from benign to very hostile.
The environmental conditions and test procedures defined herein are intended to
determine only the performance of the airborne equipment under these environmental
conditions and are not intended to be used as a measure of service life of the airborne
equipment subjected to these tests.
Any regulatory application of this document is the sole responsibility of appropriate
governmental (regulatory) agencies.
1.1
Historical Note, and General Guidance to Users
DO-160 (or its precursor, DO-138) has been used as a standard for environmental
qualification testing since 1958. It has been referenced in Minimum Operational
Performance Specifications (MOPS) for specific equipment designs, and is referenced in
FAA Advisory Circulars as a means of environmental qualification for TSO authorization.
It has been subject to a continuous process of upgrade and revision as new needs arose
within the aviation community, as improved test techniques have emerged, and as the
realities of equipment operation of under actual environmental conditions has become
better understood.
Environmental stresses can result from natural forces or man made effects, and may be
mitigated by details of the equipment installation. The categories that have been
Copyright RTCA, Inc.
Provided by IHS under license with RTCA, Inc.
Licensee=BAE Birtley, Glascoed/5932949024, User=sam, albett
Not for Resale, 03/21/2016 06:55:50 MDT
No reproduction or networking permitted without license from IHS
–“,`,“,`,“,“,,,`,,,,`,`,,`,-`-`,,`,,`,`,,`—
info@GigaPaper.ir
1-3
© 2010 RTCA, Inc.
developed over time reflect a reasonably mature understanding as to the severity of the
stresses, the degrees of mitigation achievable in the design of an installation, and the
robustness that must be designed into equipment in order to perform under the resultant
stress. In order to fully reap the advantages of the maturity of this document, it is
incumbent upon the designers of the installed equipment, as well as the designers of the
host installation, to consider the categories defined herein as early in their programs as
feasible. The categories defined within each environmental test procedure have proved to
be a practical set of boundary conditions between the requirements of real world
installations and the performance of installed equipment. Effective dialogue between the
airframe and equipment designers is essential to ensure that correct categories are utilized.