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MIL-STD-810 Altitude and Low Pressure Testing Checklist

A comprehensive checklist for conducting and evaluating altitude and low pressure tests on aerospace and defense equipment in compliance with MIL-STD-810 requirements.

MIL-STD-810 Altitude and Low Pressure Testing Checklist

by: audit-now
4.4

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About This Checklist

The MIL-STD-810 Altitude and Low Pressure Testing Checklist is a critical tool for aerospace and defense manufacturers to ensure their equipment can perform reliably in high-altitude and low-pressure environments. This specialized checklist addresses the unique challenges faced by aircraft, spacecraft, and high-altitude military equipment, focusing on the effects of reduced air pressure, temperature variations, and oxygen levels. By systematically evaluating a product's performance under these extreme conditions, this checklist helps identify potential failures, validate design integrity, and ensure operational readiness for missions in high-altitude and space environments.

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Industry

Aerospace and Defense

Standard

MIL-STD-810 - Environmental Testing

Workspaces

Laboratories

Occupations

Aerospace Engineer
Environmental Test Specialist
Avionics Systems Engineer
Pressure Systems Analyst
Space Systems Engineer
1
What is the model number of the equipment being tested?
​
2
What temperature range (in degrees Fahrenheit) was used during the environmental simulation?
​
Min: -40
Max: 185
3
Was the humidity level maintained within the specified limits during the testing?
4
Please provide any notes or comments regarding the testing procedure.
​
5
What was the completion date of the environmental simulation test?
​
6
What was the outcome of the environmental simulation test?
7
Where was the decompression test conducted?
​
8
What was the rate of decompression (in feet per minute)?
​
Min: 0
Max: 1000
9
What were the results of the decompression test?
10
Please list any safety precautions taken during the decompression testing.
​
11
When did the decompression test start?
​
12
When did the decompression test end?
​
13
Who was the lead engineer for the high-altitude performance test?
​
14
What was the total duration of the test (in hours)?
​
Min: 0
Max: 48
15
Did the equipment comply with altitude performance specifications?
16
Please document the environmental conditions during the test.
​
17
What was the date of the high-altitude performance test?
​
18
What is the overall assessment of the high-altitude performance test?
19
What is the identifier for the altitude simulation chamber?
​
20
When was the last maintenance performed on the altitude simulation chamber?
​
21
What is the current maintenance status of the altitude simulation chamber?
22
Please provide any notes regarding the maintenance performed.
​
23
What is the calibration check frequency (in months) for the chamber?
​
Min: 1
Max: 12
24
When is the next scheduled maintenance for the altitude simulation chamber?
​
25
Auditor Name
​
26
Site/Location
​
27
Date
​

FAQs

The checklist covers a range of altitudes, typically from sea level to 100,000 feet or higher, simulating conditions from ground level to the edge of space.

The checklist includes tests that simulate the combined effects of low pressure and extreme temperatures, as these often occur simultaneously at high altitudes.

Equipment tested includes avionics systems, life support systems, pressurized containers, sealed components, and any hardware intended for use in aircraft, spacecraft, or high-altitude military applications.

The checklist includes specific tests for rapid decompression, simulating sudden pressure changes that can occur during aircraft emergencies or space vehicle malfunctions.

While primarily designed for military standards, many commercial aerospace manufacturers also use or adapt this checklist to ensure their products meet similar rigorous standards for high-altitude operations.

Benefits of MIL-STD-810 Altitude and Low Pressure Testing Checklist

Ensures compliance with MIL-STD-810 altitude and low pressure testing requirements

Validates equipment functionality in high-altitude and space environments

Identifies potential issues related to pressure differentials and material outgassing

Improves safety and reliability of aerospace and defense systems

Supports the development of robust designs for extreme environmental conditions