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authorMarius Peter <marius.peter@tutanota.com>2022-03-26 19:02:15 +0100
committerMarius Peter <marius.peter@tutanota.com>2022-03-26 19:02:15 +0100
commitdf5862d950eb9c63f50363220bf38bfc24d530c9 (patch)
treeb58a74c0049466717facfc1a94568d2f470cb28f /wiki/aerospace/standard
parent95c3ce4bc795d6582a09467c9fb60b639a8c9f46 (diff)
Wiki articles.
Diffstat (limited to 'wiki/aerospace/standard')
-rw-r--r--wiki/aerospace/standard/ARP4754.org36
-rw-r--r--wiki/aerospace/standard/DO-160.org108
2 files changed, 144 insertions, 0 deletions
diff --git a/wiki/aerospace/standard/ARP4754.org b/wiki/aerospace/standard/ARP4754.org
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+# -*- mode: org; -*-
+
+#+TITLE: ARP4754
+#+SUBTITLE: Guidelines For Development Of Civil Aircraft and Systems.
+#+AUTHOR: Marius Peter
+#+DATE: <2022-02-11 Fri>
+#+EMAIL: mlnp@tuta.io
+#+OPTIONS: toc:nil
+
+#+KEYWORDS: aerospace, SAE, ARP 4754
+
+#+TOC: headlines 2
+
+
+#+begin_abstract
+ARP4754 is a guidance issued by SAE.
+#+end_abstract
+
+
+* Introduction
+
+ https://www.sae.org/standards/content/arp4754a/
+
+
+* Main topics
+
+| § | Theme | Description |
+|---+---------------------+-------------|
+| 1 | Development | |
+| 2 | Safety | |
+| 3 | Requirements mgmt. | |
+| 4 | Validation | |
+| 5 | Verification | |
+| 6 | Configuration mgmt. | |
+| 7 | Process assurance | |
+| 8 | Certification | |
diff --git a/wiki/aerospace/standard/DO-160.org b/wiki/aerospace/standard/DO-160.org
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+# -*- mode: org; -*-
+
+#+TITLE: DO-160
+#+SUBTITLE: Environmental Conditions and Test Procedures for Airborne Equipment.
+#+AUTHOR: Marius Peter
+#+DATE: <2022-02-11 Fri>
+#+EMAIL: mlnp@tuta.io
+#+OPTIONS: toc:nil
+
+#+DESCRIPTION: Environmental Conditions and Test Procedures for Airborne Equipment.
+#+KEYWORDS: aerospace, rtca, DO-160
+
+
+#+TOC: headlines 2
+
+
+#+begin_abstract
+The DO-160 document is a standard for environmental testing for
+airborne equipment published by the RTCA.
+#+end_abstract
+
+
+* Introduction
+
+ https://do160.org/rtca-do-160g/
+
+
+* Equipment categories
+
+Equipments are categorized as a function of the environments to which
+they are subjected during normal operation.
+
+
+* Sections
+
+Sections 7 and 8 are aircraft dependent.
+
+
+** List
+:PROPERTIES:
+:HTML_CONTAINER_CLASS: big-table
+:END:
+
+#+NAME: sections
+#+CAPTION: List of DO-160 section.
+| § | Name | Concerns the effects of... | Parameters of interest |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 1 | /Introductory sections/ | /N/A/ | /N/A/ |
+| 2 | | | |
+| 3 | | | |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 4 | Temperature | Temperature on the system. | Temperature, condensation. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 4 | Altitude | Altitude & cabin depressurization on performance. | Dielectric strength, (rapidly) varying air pressure. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 5 | Temperature Variation | Extreme temperature changes. | Temperature delta, thermal expansion coefficients. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 6 | Humidity | High concentrations of humidity; ability to withstand moisture effects.[fn:1] | Hygrometry. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 7 | Shock & Crash safety | Mechanical shock. Ensures the item does not become a projectile in a crash. | Potential for projectile behavior. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 8 | Vibration | Vibrations. | Normal operation in all vibration scenarios. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 9 | Explosion proofness | Vacuum + gaseous mixture of combustibles. | The unit must be operable without igniting the environment. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 10 | Water proofness | Dripping water or pooled water. | Normal operation after exposure. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 11 | Fluids susceptibility | Various fluids including carbonated sugared beverages and cleaners/solvents. | Normal operation after exposure. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 12 | Sand & Dust | Blowing sand and dust of specific particle sizes. | Normal operation after exposure. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 13 | Fungus Resistance | Fungi under conditions favorable for their development.[fn:3] | Fungal proliferation. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 14 | Salt & Fog | Multiple exposures of salt fog and drying; environmentally accelerated corrosion. | Normal operation after exposure. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 15 | Magnetic effect | Magnetic effects on the aircraft's compass. | Normal aircraft compass function. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 16 | Power input | Input power emissions, susceptibility, transients, drop-outs, hold-up.[fn:2] | Voltage, current, phase. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 17 | Voltage spike | Voltage spikes caused by input power. | AC/DC voltage. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 18 | Audio Frequency Conducted Susceptibility | Frequency components during normal operation. | Power source harmonics. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 19 | Induced Signal Susceptibility | Induced voltages in the equipment interconnect circuit configuration. | power frequency harmonics; audio frequency signals, electrical transients. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 20 | RF emission and susceptibility | Normal operation on radio frequency emission energy and susceptibility. | |
+| 21 | | | |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 22 | Lightning susceptibility | Direct and indirect effects, depending on location. | induced transients in the airframe or wire bundle. |
+| 23 | | | |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 24 | Icing | Icing conditions arising from rapid changes in temperature, altitude and humidity. | Presence of ice. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 25 | ESD | ESD in handling and operation. | ESD. |
+|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
+| 26 | Flammability | Normal operation on presenting a fire hazard. | Normal operation not causing a fire. |
+
+
+* Footnotes
+
+[fn:3] This includes high humidity, a warm atmosphere, and the
+presence of inorganic salts.
+
+[fn:2] Full flight mission must be considered, from prior to the
+engine start, to after landing---including emergencies.
+
+[fn:1] Moisture sensitive devices may experience issues with this test
+and require conformal coat or other types of protection.
Copyright 2019--2026 Marius PETER