MIL-STD-810 – the ideal tool for demanding environments

Ett flygplans som lyfter
En grön militärlastbil

MIL-STD-810

MIL-STD-810 is a comprehensive standard developed by the U.S. Department of Defense for environmental engineering considerations and laboratory testing. It contains guidelines for testing mainly military equipment, electronics and components in the aerospace industry under various environmental conditions to ensure reliability and durability in harsh environments. The standard covers methods for testing the effects of temperature, humidity, vibration and altitude on equipment. The focus is on adapting the test procedures to specific equipment and application profiles to ensure that the tests are relevant and effective. Many standards can be met with testing equipment from weisstechnik.

We offer the right solution for every test specimen – from compact bench-top models with 16 liters of test chamber volume, to reach-in test chambers, to drive-in systems for large-volume applications. In addition to our standard products, we work with our customers to develop customized solutions that are precisely tailored to specific requirements.

Industries & Applications

Industries & Applications – Where MIL-STD-810 makes the difference

Aerospace

From avionics systems and onboard electronics to satellite components, products used in aviation must withstand pressure changes, temperature fluctuations, vibrations, and radiation. MIL-STD-810 provides the basis for the qualification of these components.

Defense & Security

Military equipment must meet the highest standards of reliability under extreme conditions – from the desert to the Arctic, from jumping out of aircraft to transport in armored vehicles. MIL-STD-810 serves as the authoritative testing standard in this context.

Typical test specimens: Communication systems, vehicle electronics, portable equipment, sensor technology.

Electronics & Industrial Electronics

Electronic components for outdoor and industrial applications must remain functional at all times – even when exposed to heat, moisture, corrosion, or mechanical stress. MIL-STD-810 ensures operational readiness even in extreme scenarios.

Typical test specimens: Control units, displays, IoT components, embedded systems.

Automotive (civilian and military vehicles)

Modern vehicles – especially in a military context – are high-performance rolling systems. Tests according to MIL-STD-810 help validate the resistance of electronics and mechanics to environmental influences.

Typical test specimens: Control devices, camera systems, displays, vehicle components.

Telecommunications

In civil and military telecommunications, devices are often used outdoors – in regions with extreme climatic conditions or in mobile operations. MIL-STD-810 defines realistic scenarios for testing these systems.

Typical test specimens: Radio equipment, mobile communications technology, network components, base stations.

En grön militärlastbil

Temperature & climate

Electronic systems, materials, and housings are often exposed to extreme cycles—from arctic cold to tropical heat and sudden temperature changes during flight or vehicle operation. The combination of static temperature and humidity tests and dynamic temperature shock simulates realistic environmental conditions. This allows condensation, material expansion, aging effects, and stress cracks to be detected as early as the development stage.

These tests are essential for manufacturers in the defense and aerospace industries, for automotive control units (civilian & military), industrial electronics, and for telecommunications and outdoor devices.

Method 501.7 High Temperature

Purpose/Summary:
Method 501.7 is used to evaluate the effects of high temperatures on the safety, integrity, and performance of military equipment during storage, operation, and tactical readiness. This method is primarily used in the defense, aerospace, and energy industries to ensure reliability under heat-intensive conditions.

Application:
e.g. viscosity, lubricants, stresses caused by different thermal expansion, mechanical damage, outgassing of composite materials and coatings, stability of electronic circuits, etc.

Test scenarios:

  • Procedure I – Storage: The material is exposed to high temperatures in a storage configuration to detect structural changes. After at least seven cycles, a functional test is performed under standard conditions.
  • Procedure II – Operation: The device is operated at constant or cyclic high temperatures. The aim is to check functionality during thermal stress, especially at maximum temperature response.
  • Procedure III – Tactical standby to operation: After exposure to maximum non-operating temperature, there is a rapid transition to operating temperature. The device must be ready for immediate use – without active cooling.

Suitable Weiss Technik products:
TempEvent or ClimeEvent (with climate range extension and compressed air dryer for humidity <10% RH), R devices, MUR and LabEvent.

  • Parameter Example values
  • Ambient air temperature (basic hot): 30 to 43 °C
  • Induced temperature (basic hot): 30 to 63 °C
  • Ambient air temperature (hot and dry): 32 to 49 °C
  • Induced temperature (hot and dry): 33 to 71 °C
  • Humidity (basic hot): 14 to 44% RH
  • Humidity (hot and dry): 1 to 8% RH
  • Temperature change rate: ≤ 3 °C/min
  • Test duration Procedure I (storage): &; 7 cycles
  • Test duration Procedure II (operation): > 3 cycles

Method 502.7 Low Temperature

Purpose/Summary:
Method 502.7 defines how to evaluate devices that are exposed to low temperatures. It outlines three key procedures—storage, operation, and handling—each of which simulates real-world exposure to cold. This standard is essential for the defense, aerospace, and energy industries to ensure reliability under cold conditions.

Application:
These include hardening and embrittlement of materials, mechanical damage or malfunctions due to varying thermal expansion, mechanical damage, lubricant failure, and performance changes in electronic components.

Test scenarios:
Various test methods for use, storage, and operational readiness. Ensuring operational readiness at low temperatures.

Cycles:
Consistent temperatures for test specimens with additional cycle at room temperature if necessary.

Suitable Weiss Technik products:
TempEvent, LabEvent, R devices and MUR

Special feature:
The recommended test duration according to MIL-STD-810H is 4 hours after stabilization for non-hazardous or non-safety-critical (non-life-sustaining) materials. Ammunition, rubber, and plastics may deteriorate further after stabilization at low temperatures. For these materials, a minimum duration of 72 hours after temperature stabilization is recommended.

  • Parameter Example values
  • Ambient air temperature (basic cold) -21 to -32 °C
  • Induced temperature (basic cold) -25 to -33 °C
  • Ambient air temperature (cold) -37 to -46 °C
  • Induced temperature (cold) -37 to -46 °C
  • Ambient air temperature (extreme cold) -57 °C
  • Induced temperature (extreme cold) -57 °C
  • Temperature change rate ≤ 3°C/min
  • Test duration (not dangerous) > 4 hours
  • Test duration (Dangerous) > 72 hours

Method 503.7 Temperature Shock

Purpose/Summary:
Method 503.7 (temperature shock) evaluates the ability of a test specimen to withstand sudden, extreme changes in ambient temperature. It simulates rapid transitions between hot and cold environments to evaluate structural integrity and operational reliability. This method is important for defense, aerospace, and industrial electronics, where devices may be exposed to abrupt temperature fluctuations during transport or use.

Application:
This method is used to identify failure mechanisms in the event of sudden, extreme temperature fluctuations. These include the breakage of sensitive components, the deformation or failure of mechanical parts due to varying thermal expansion, and the cracking of coatings or the leakage of sealed areas.

Chemically, this can lead to the separation of substances or impair protective barriers. Component properties can change electronically; condensation or frost can cause short circuits or mechanical defects.

Test scenarios:

  • Procedure I – Equipment in storage or in transit: Assessment of the risk of physical damage due to thermal shocks during non-operational phases. The device is moved back and forth between two extreme temperatures while it is not connected to a power source. The process is used for warehouse storage, air transport, and logistics without a power connection.
  • Procedure II - Equipment in operational configuration: Evaluates operational performance during or after a temperature shock. The item is supplied with power during or immediately after exposure to extreme temperatures. This is especially relevant for in-service systems, mission-critical electronics, and aerospace avionics.

Cycles:
Single cycles or multiple cycles

Suitable Weiss Technik products:
ShockEvent T or D (flap shock); for higher weights, TempEvent with > 10 K/min

Special feature:
Test Setup

  • Use two temperature chambers or a single chamber with two zones. Ensure a rapid transition between the hot and cold zones (preferably ≤ 1 minute). Monitor the internal temperature of the test object.
  • If test specimens with greater weight are being tested, it may be necessary to use the two-chamber method. The test specimen is moved using a pallet truck (temperature change then > 1 minute).

  • Parameter Example values
  • Temperature limits Based on climate categories (e.g., -51°C to +71°C)
  • Transfer time between chambers ≤ 1 minute (typical)
  • Number of cycles 3 to 5 (standard), up to over 20 for extended tests
  • Stabilization period Until the chamber’s internal temperature is reached
  • Relative Humidity It is not controlled except in cases where there is a risk of condensation

Method 507.5 Humidity

Purpose/Summary:
The “humidity” method describes procedures for testing the resistance of materials to warm, humid environments. It comprises two main processes: induced (storage and transport) and natural cycles, each simulating different humidity conditions. This method is crucial for industries such as defense, aerospace, and electronics, where the reliability of equipment under humid conditions is critical.

Application:
For oxidation, chemical reactions, interaction between condensation and coatings, changes in physical properties (e.g., delamination, degradation of explosives and propellants due to absorption), and short circuits

Test scenarios:

  • Procedure I - Induced (storage & transit): This procedure evaluates the resistance of the material to moisture during storage and transport, as well as under natural environmental conditions.
  • Procedure II (enhanced procedure): This procedure is designed to produce representative effects that typically occur under elevated temperature and humidity conditions, without precisely replicating naturally occurring conditions.

Suitable Weiss Technik products:
ClimeEvent

  • Parameter Example values
  • Temperature range 24 °C to 71 °C
  • Relative Humidity 14% to 100% RH
  • Test duration 10 to 180 cycles (days)
  • Air velocity 0.5 to 1.7 m/s
  • Chamber control accuracy > ±0.6°C
En maskin som sprutar vatten

Water and liquids

Penetrating water and aggressive liquids (oils, fuels, cleaning agents) can cause short circuits in electronics, accelerate corrosion, or damage seals. Water and liquid tests assess the sealing and protection concepts of enclosures, connectors, and assemblies under real-world operating conditions. Standardized test setups for tropical rain, direct jet water exposure, as well as short-term and prolonged liquid exposure are used for testing. Industries such as defense, aerospace, automotive (civil & military), industrial electronics, and telecommunications use these tests for displays, control units, sensors, pumps, and valves. The results help optimize enclosure designs and sealing systems for full functionality under water and liquid exposure.

Method 506.6 Rain

Purpose/Summary:
This method is used to determine the effectiveness of protective covers, enclosures, and seals against water ingress, the ability of the material to meet performance requirements during and after exposure to water, and to evaluate physical damage and the efficiency of water removal systems. It is applicable to materials that may be exposed to rain, splashing water, or dripping water during storage, transport, or operation. The method comprises three main procedures for realistically simulating various rain conditions in military applications

Application:
This method is used in the defense industry to evaluate military equipment that may be exposed to rain, splash water, or dripping water during storage, transport, or operations.

Test scenarios:

  • Procedure I (rain & driving rain): This procedure is used to simulate the effects of natural rain and rain driven by wind. It evaluates how well the material withstands direct exposure to water and water penetration.
  • Procedure II (exaggerated): This procedure is designed for simulating more extreme water jets or sprays, such as those produced by moving vehicles or high-pressure cleaning systems.
  • Procedure III (drops): This procedure is suitable when the material is normally protected from rain but may be exposed to falling water from condensation or leaks from upper surfaces.

Suitable Weiss Technik products:
WaterEvent

  • Parameter Example values
  • Rain/drop spray rate Procedure I (rain & driving rain): > 1.7 mm/min (4 in/h) measurements on average within 10% or +/- 0.1 mm/min (0.25 in/h) of the target value, each measurement within 25% or +/- 0.2 mm/min (0.5 in/h) of the target value.

    Procedure II (Exaggerated): Nozzle pressure 276 kPa, flow rate 20.8 liters/min, droplet velocity approx. 64 km/h (40 mph).

    Procedure III (drops): > 280 liters/m²/h dripping; alternatively 140 liters/m²/h with 30 minutes extended duration.
  • Droplet size Procedure I: Mainly between 500 µm and 4500 µm in diameter.
  • Drip pattern Procedure III: 20–25.4 mm
  • Drip height Procedure III: > 1 meter above the upper main surface of the test specimen.

Method 521.4 Icing Freezing Rain

Purpose/Summary:
The purpose of this method is to evaluate the effects of icing on the operational performance of equipment and to assess the effectiveness of de-icing devices and techniques (including those available in the field). It applies to equipment that may be exposed to icing due to freezing rain, freezing drizzle, or fog, as well as to ice formation due to splashing or spraying sea water. The method focuses on determining whether the equipment remains operational after ice accumulation or whether de-icing procedures can be successfully applied.

Application:
This method is primarily relevant to the defense industry for testing military equipment used in cold and humid environments where icing due to freezing rain, drizzle, fog, or sea spray may occur.

Test scenarios:
Procedure (ice accumulation): This procedure involves icing the test specimen under controlled conditions. It involves installing the test specimen in a refrigerated chamber and spraying it with supercooled water to produce ice accumulation.

Suitable Weiss Technik products:
ClimeEvent (with optional equipment)

  • Parameter Example values
  • Chamber temperature -10 °C to -2 °C
  • Spray system water temperature 0 °C to 3 °C
  • Initial temperature of the test specimen > 0 °C
  • Duration of ice hardening > 4 hours

Method 524.1 Freeze / Thaw

Purpose/Summary:
Method 524.1 determines the ability of material to withstand the effects of moisture phase changes (between liquid and solid) in or on the material as it cycles through the freeze point. It also evaluates the effects of moisture induced by transfer from a cold to a warm environment or from a warm to a cold environment. The method is not intended for evaluating low temperatures, thermal shock, rain, or icing, but focuses on the physical changes caused by repeated freeze-thaw cycles.

Application:
This method is relevant for the defense industry and materials used in environments where moisture is present and temperatures repeatedly exceed or fall below freezing.

Test scenarios:

  • Procedure I (daily cycles): Simulates the effects of daily temperature fluctuations just above and below freezing, typical of daytime warming and nighttime freezing when ice deposits, condensation, or high relative humidity are present.
  • Procedure II (fogging): This procedure simulates the effects of moisture induced by transfer from a cold to a warm environment.
  • Procedure III (rapid temperature change): This procedure simulates the effects of rapid temperature changes that can lead to freezing and melting.

Suitable Weiss Technik products:
ClimeEvent (with optional equipment), LabEvent

  • Parameter Example values
  • Temperature range Procedure I: -10 °C to +5 °C

    Procedures II & III: -10 °C to standard ambient temperature
  • Temperature ramp rate (procedure I) < 3 °C/min
  • Humidity Water as water vapor or splashing water
  • Number of cycles Procedure I: > 20

    Procedure II: 3

    Procedure III: 3
  • Hold time per state More than one hour after temperature stabilization of the test specimen
  • Transfer time (between chambers) < 5 minutes
  • Relative humidity (procedure III) 95 ± 5 % at the upper temperature
Corrosion chamber

Corrosion

Salt, moisture, and chemical aggressors attack metal structures, contacts, and sealing systems over time. Unprotected hardware can become inoperable within weeks, especially in marine, coastal, or industrial environments. To prevent this, corrosion tests accelerate aging processes and provide reliable information on the effectiveness of coatings, alloys, and sealing solutions.

MIL‑STD‑810 Method 509 defines salt fog and humidity chamber tests that realistically simulate salty and humid climates. Defense and aerospace manufacturers test structural components, connectors, and housings, as well as automotive components (civilian & military) and industrial electronics. Telecommunications providers test outdoor antenna locations and base stations to validate corrosion protection measures. Result: long-lasting product reliability and reduced maintenance cycles.

Method 509.8 Salt Fog / Corrosive Environments

Purpose/Summary:
The purpose of this method is to determine the effectiveness of protective coatings and surface treatments for protecting materials in saline environments. It is also used to determine the effects of salt spray, salt deposits, moisture, humidity, and temperature fluctuations on the physical and electrical aspects of materials. The method produces a test load that can reveal potential material problems, but is not intended to predict service life. Three procedures are available, which can be tailored to the test objectives and the environment to be simulated.

Application:
This method is crucial in the defense industry for the development and testing of materials used in saline environments, such as marine applications or coastal areas. It is relevant for protective coatings and surface treatments.

Test scenarios:

  • Procedure I (corrosion screening): This procedure is used exclusively for screening purposes to evaluate the effectiveness and quality of protective coatings and surface treatments on materials and material coupons and to identify potential problem areas, quality control deficiencies, design flaws, etc. in a relatively short period of time.
  • Procedure II(Corrosion verification design): Corrosion verification design: This procedure is used to verify the corrosion resistance of system designs during the engineering phase of acquisition.
  • Procedure III (natural environment): Natural environment: This method involves outdoor exposure tests in the natural environment, typically over a period of at least 12 months in a coastal marine environment.

Suitable Weiss Technik products:
SaltEvent SC-H, Ascott Cyclic Corrosion Chambers

  • Parameter Example values
  • Salt solution concentratio Procedure I: 5 ± 1 percent by weight sodium chloride (NaCl)
  • Water temperature (chamber) 35 ± 2 °C
  • Pre-temperature (compressed air) Varies depending on air pressure, e.g. 46 °C at 83 kPa, 49 °C at 124 kPa (49 psi).
  • Relative Humidity < 50% RH
  • Duration Procedure I (corrosion screening): Cycles of 24 hours of exposure and 24 hours of drying, or 48 hours of exposure and 48 hours of drying.

    Procedure II (corrosion verification design): Typical laboratory tests range from 336 hours to 2000 hours of continuous exposure; for marine aviation, a minimum of 2016 hours (ASTM B117) is required, with 504 hours of continuous ASTM B117 exposure being standard.

    Procedure III (natural environment): At least 12 months of exposure in a coastal marine environment.
  • Water resistance 0.2 megaohms cm for salt solution and rinse water.
  • Sample orientation (method III) Typically 45° to the horizontal plane
Light & radiant exposure

Light & radiant exposure

UV radiation, visible light, and infrared rays from the sun cause surface aging, color changes, embrittlement, and temperature hot spots. Solar simulation tests long-term stability and thermal stress caused by solar radiation.

MIL‑STD‑810 Method 505 specifies measurement parameters for spectrally correct radiation and intensity. Application in defense and aerospace projects, automotive exterior panels (civil & military), industrial outdoor installations, and telecommunications antennas. Enclosure materials, optics, sensor windows, and solar cells are tested for UV resistance, thermal stability, and embrittlement resistance, ensuring product quality in outdoor applications.

Method 505.7 – Solar Radiation (Sunshine)

Purpose/Summary:
MIL-STD-810 Method 505.7 describes procedures for evaluating the effects of solar radiation on materials and equipment. It focuses on both the heating and actinic (photodegradation) effects of solar radiation and ensures that materials can withstand prolonged exposure to sunlight without significant deterioration.

Application:
e.g., jamming or loosening of moving parts, weakening of solder joints and bonded parts, changes to electrical or electronic components, softening of casting compounds, etc. Changes in strength and elasticity.

Test scenarios:
Preliminary test for baseline, cyclic test, and test under constant conditions.

Suitable Weiss Technik products:
SunEvent (for 600 and 1000 liters: method 1 with adjustments possible (daily cycle), method 2 possible as standard)

Special feature:
Different test scenarios for specimens that are frequently or occasionally outdoors. Varying intensities throughout the day. The customer must provide a spectrometer and an air flow sensor. The device must be used with a CM4 pyranometer and the adjustable recirculation volume option.

  • Parameter Example values
  • Maximum radiation level 1120 W/m²
  • Test duration Variable (3 to 7 cycles for procedure I, up to 56 cycles for procedure II)
  • Air velocity 1.5 to 3.0 m/s
  • Temperature control ±2 °C

Suitable products for your selection

Light & radiant exposure

Particles and atmospheric influences

Dust, sand, and contaminated air particles can block fans, contaminate sensors, and cause heat build-up. Explosive or toxic atmospheres pose additional risks. Realistic particle testing is therefore essential.

MIL‑STD‑810 Method 510 (Dust/Sand) defines test chamber conditions for fine particle emissions. Defense and aerospace developers, automotive vehicle systems (civil & military), industrial installations, and telecommunications base stations are validated for particle tightness, filter efficiency, and explosion safety. This ensures system functionality even in desert, industrial, or urban operational environments.

Method 510.7 Sand and Dust

Purpose/Summary:
MIL-STD-810 Method 510.7 is used to assess the resistance of materials to sand and dust environments, tailored to specific environmental conditions and material requirements. This method is relevant for a wide range of mechanical, optical, electrical, electronic, electrochemical and electromechanical devices in industries where such exposures are expected.

Application:
Method 510.7 is used to test the functionality and durability of equipment in sand- and dust-prone environments—such as desert regions, military operations, aerospace, power supply, or off-road vehicles. It is crucial not only for protection against mechanical abrasion and clogging, but also for preventing electrical malfunctions caused by conductive dust particles or thermal overload from blocked ventilation systems.

Test scenarios:

  • Procedure I (Blowing Dust): Evaluates the material’s ability to withstand dust that can clog openings, penetrate cracks, crevices, bearings, and joints, as well as assess the effectiveness of filters.
  • Procedure II (Blowing Sand): Evaluates the material’s ability to be stored and operated under these conditions without performance, effectiveness, reliability, or maintainability being impaired by abrasion (erosion) or clogging from sharp-edged particles.

Suitable Weiss Technik products:
Dust test chamber DustEvent

  • Test parameter
  • Particle size Procedure I: Blowing Dust: < 150 µm
    Procedure II: Blowing Sand: 150 µm to 850 µm
  • Median particle diameter Procedure I: Blowing Dust: 20 ±5 µm (at 100% < 150 µm)
    Procedure II: Blowing Sand: 90 ±5% between 150 µm and 600 µm, min. 5% >= 600 µm
  • Temperature Procedure I: Blowing Dust: Standard ambient temperature and high operating or storage temperature; max. ambient temperature for climate category A1
    Procedure II: Blowing Sand: High operating or storage temperature; max. ambient temperature for climate category A1
  • Relative humidity (RH) Procedure I: Blowing Dust: ≤ 30 percent
    Procedure II: Blowing Sand: Not specific to sand, but test environment is relatively dry
  • Air velocity Procedure I: Blowing Dust: Reduced: 1.5 ±1 m/s, Higher: 8.9 ±1.3 m/s
    Procedure II: Blowing Sand: Standard: >18 m/s, Gusts: < 29 m/s
  • Wind speed sampling rate Procedure I: Blowing Dust: > 4 samples/second
    Procedure II: Blowing Sand: Standard: > 4 samples/second
  • Dust/sand composition Procedure I: Blowing Dust: Recommended: Natural dust from the region; Alternatively: Red Chinese sand (e.g. 50-80% SiO2, 20 ±10% Al2O3, 10 ±5% Fe2O3); or silica flour (97-99% SiO2)
    Procedure II: Blowing Sand: Standard: Quartz sand (at least 95% SiO2), sub-angular structure, Krumbein number 0.5-0.7, hardness 7 Mohs
  • Temperature change rate Procedure I: Blowing Dust: < 3°C/min during transition
    Procedure II: Blowing Sand: < 3°C/min during transition

Suitable products for your selection

Altitude and pressure conditions

Altitude and pressure conditions

At high altitudes or during rapid pressure changes (e.g., flight, mountain driving, UAV use), the ambient pressure drops, which can impair the functionality of seals, ventilation systems, and electrical components. Vacuum scenarios in aerospace and high-altitude research are also covered.

MIL‑STD‑810 Method 500 describes the simulation of altitudes up to 12,000 m and rapid pressure changes. Defense, aerospace, and UAV manufacturers, as well as automotive suppliers (civil & military) and industrial facilities, use this method to plan pressure tests for sensors, batteries, cable feedthroughs, and cooling systems. In telecommunications, high-altitude repeaters and weather stations are validated. Objective: Prevent vacuum lock, gas evolution in batteries, and seal failure.

Method 500.6 Low Pressure (Altitude)

Purpose/Summary:
MIL-STD-810 Method 500.6 is used to assess the resistance and functionality of materials in low-pressure environments or under rapid air pressure changes. It includes four specific test procedures, which must be carefully tailored to the intended lifecycle of the material.

Application:
The applicability mainly extends to materials stored, transported, or operated in aviation, as well as those that may be exposed to extreme decompression. It is used for materials likely to be stored and/or operated at high-altitude locations, transported or operated in pressurized or unpressurized areas of aircraft, exposed to rapid or explosive decompression, or carried externally on aircraft.

Limitation:
This method is not intended for materials to be installed or operated in spacecraft, aircraft, or rockets flying at altitudes above 21,300 m.

Test scenarios:
Method 500.6 comprises four different low-pressure test procedures: storage/air transport, operation/air transport, rapid decompression, explosive decompression

Suitable Weiss Technik products:
SkyEvent

  • Parameter Example values
  • Maximum Test Altitude (Limitation) 21,300 m
  • Maximum Ground Altitude (Military) 4,572 m (57.2 kPa)
  • Cabin pressure (standard for procedures I & II) 4,572 m (57.2 kPa)
  • Initial cabin pressure (standard for procedures III & IV) 2,438 m (75.2 kPa)
  • Final cabin pressure after decompression (standard for procedures III & IV) 12,192 m (18.8 kPa)
  • General altitude change rate 10 m/s
  • Average altitude change rate (military transport aircraft) 7.6 m/s
  • Explosive decompression rate < 0.1 seconds
  • Rapid decompression rate < 15 seconds
  • Minimum duration (procedure I) < 0.1 seconds
  • Temperature change rate (chamber) 3 °C/min
  • Duration at reduced pressure (procedures III & IV) 10 minutes
Combination tests & special methods

Combination tests & special methods

Environmental conditions rarely occur in isolation: heat combined with humidity, temperature shock under low pressure, or vibration with sand exposure are typical combinations. MIL‑STD‑810 allows modular test sequences and special tests that realistically simulate complex operational scenarios.

Manufacturers in the defense, aerospace, automotive, industrial electronics and telecommunications industries use combined tests to validate complete system integration, whether for drones, armored vehicles, mobile command units, offshore base stations or space systems. Special methods such as MIL‑STD‑810 Method 502.6 (combined humidity) or customer-specific test procedures support customized requirements and ensure maximum availability under multiple loads.

Method 520.5 Combined Environments

Purpose/Summary:
The purpose of this method is to determine the synergistic effects of combinations of temperature, altitude, humidity, electrical input power, and vibrations on aircraft-grade electronic and electromechanical material during ground and flight operations. These tests are designed to detect failures that would not occur in single environment tests. The method is primarily intended for actively propelled material at altitude and can be used for technical development, flight or mission support.

Application:
This method is mainly tailored to the defense industry, especially for aviation and missile electronics/electromechanics and mission equipment. It can also be adapted for use on ground vehicles, support equipment, and human-worn equipment.

Test scenarios:

  • Procedure I (development, procedure): This procedure is used during technical development to identify design flaws in new or modified devices.
  • Procedure II (flight/mission): This procedure aims to simulate the climatic, dynamic, electrical input power, and operating events of specific missions or troubleshooting scenarios.
  • Procedure III (platform envelope): This procedure is used to demonstrate compliance with specific platform/equipment specification requirements under combined synergistic environmental conditions.

Suitable Weiss Technik products:
SkyEvent, ClimeEvent

  • Parameter Example values
  • Combination of environments Temperature, altitude, humidity, electrical input power, and vibration (three or more simultaneously).
  • Temperature ramp rate ≤5 °C/min
  • Humidity ramp rate Must be sufficient to induce condensation and/or frost, e.g. when descending from high altitude/cold to low altitude/warmth/humidity. Can be delayed until the chamber temperature reaches 0 °C.
  • Altitude ramp rate According to the platform's performance.
  • Test duration Procedure I (development): Based on the time required to induce expected fault modes. Procedure II (flight/mission): Representative of the design mission or sufficient for troubleshooting. Procedure III (platform envelope): At least 10 cycles. Duration sufficient for thermal stabilization and representative of the LCEP.
  • Electrical input power Normal range: AC: 107.5-119.5 Vrms (older MIL-STD-704 versions) to 108-118 Vrms (newer versions); frequency 380-420 Hz or 393-407 Hz. DC (ground vehicles): 20-33 VDC (MIL-STD-1275E). Abnormal range: AC: 100-137 Vrms; frequency 320-480 Hz. Emergency range: AC: 102-124 Vrms; frequency 360-440 Hz. Recommended test cycle for voltage and frequency.
  • Vibration level Derived from measured data or method 514

Method 511.5 Explosive Atmosphere

Purpose/Summary:
MIL-STD-810 Method 511.5 describes procedures for evaluating the safety and performance of materials in explosive atmospheres. It ensures that equipment can be operated without igniting the explosive gases or vapors surrounding it, which is critical for safety in various industries, including defense, aerospace, and energy.

Application:
Aircraft avionics, fuel system components, maintenance tools.

Test scenarios:

  • Procedure I – Ignition test in explosive atmosphere: The test specimen is placed in a sealed chamber filled with a controlled mixture of air and n-hexane vapor. The test specimen shall be operated under normal conditions and any ignition shall be detected. This determines whether the test specimen can operate in a flammable atmosphere without igniting it.

Suitable Weiss Technik products:
ExtremEvent

Special feature:
Tests in this area are highly complex. Get in touch and one of our specialists will talk you through the details of the test and the technical possibilities.

  • Parameter Example values
  • Dew point in the test chamber Below 10 °C
  • Simulated altitude Up to 2000 m above ambient pressure
  • Fuel vapor used n-Hexane (standardized explosive vapor)
  • Ignition source Internal spark or thermocouple
  • Explosion detection Thermocouple or pressure sensor
  • Test repetitions Up to 5 cycles (depending on the volume of the specimen)
Mechanical stress

Mechanical stress

Transport, shock loads during landing or combat situations, and constant vibrations during vehicle or aircraft operation place heavy demands on electronics and mechanics. Mechanical tests reveal possible fractures, loosening of connections, and material fatigue.

MIL‑STD‑810 Method 514 (Vibration) is relevant across industries for defense, aerospace, automotive (civilian & military), industrial electronics, and telecommunications. The tests cover printed circuit boards, connectors, displays, housings, mounting systems, and structural components. Results are incorporated into design optimizations and assembly guidelines to increase robustness.

Method 514.8 Vibration

Purpose/Summary:
The purpose of this method is to provide guidance on the definition of vibration environments to which material may be exposed during its life cycle and guidance on the performance of laboratory vibration tests. These tests are designed to ensure that the material functions and withstands the vibration stresses of a life cycle, including synergistic effects of other environmental factors. The method offers four specific procedures for simulating various vibration scenarios to which military equipment is exposed.

Application:
This method is widely applicable in the defense industry, as virtually all military materials are subject to vibrations during manufacture, transport, maintenance, or operation. This includes ground transport (trucks, trailers, tracked vehicles), air transport (jet and propeller aircraft, helicopters), sea transport, rail transport, personnel-carried equipment, and power plant installations.

Test scenarios:

  • Procedure I (general vibration): Used for material that is transported as secured freight or used on a vehicle.
  • Procedure II (transport of loose cargo): This procedure applies to material that is transported in trucks, trailers, or tracked vehicles and is not secured (not tied down).
  • Procedure III (Transport of large assemblies): This procedure is designed to replicate the vibration and shock loads experienced by large assemblies installed in or transported by wheeled or tracked vehicles.
  • Procedure IV (Mounted aircraft external loads): This procedure applies to mounted external loads that are attached to aircraft or in free flight.

Suitable Weiss Technik products:
ShakeEvent

  • Parameter Example values
  • Frequency range (Aircraft) >10 Hz. (Below 10 Hz, it is assumed that the cargo does not react dynamically.)
  • Movement (Procedure II, Loose Load) 25.4 mm, Circular synchronous movement at 5 Hz.
  • Exponent ‘m’ (Miner-Palmgren hypothesis) Typically between 5 and 8 for random vibrations; 6 for sinusoidal vibrations. Specific values for steel and aluminum alloys.
  • General minimum integrity (Annex E) Duration: One hour per axle. RMS: 7.7 g
  • Temperature during the test Standard environmental conditions, but can be adjusted to life cycle events.

White paper with measured data