Altitude & Low-Pressure Testing — DO-160 Section 4 and MIL-STD-810 Method 500.6.

As altitude rises, air pressure falls — and that single change stresses equipment in several ways at once: seals and gaskets leak, trapped air and fluids escape, the thinner air carries away less heat so electronics run hotter, and reduced dielectric strength makes arcing easier. Two frameworks define how to verify it: DO-160 Section 4 for civil airborne equipment, and MIL-STD-810 Method 500.6 for defense materiel.

Why low pressure matters

• Reduced cooling. Thinner air convects less heat, so components that ran cool at sea level can overheat at altitude.
• Leakage and fluid loss. Pressure differentials drive air and fluids out through seals, gaskets and vents.
• Electrical effects. Lower dielectric strength makes arcing and corona more likely across gaps and contacts.
• Decompression damage. A rapid drop in pressure can rupture sealed enclosures or distort components.

DO-160 Section 4 (Temperature and Altitude)

Section 4 is DO-160's signature test: it combines temperature extremes with reduced pressure to reproduce flight, rather than testing either alone. Categories range from mild pressurized-cockpit conditions (around −15 °C to +55 °C) to severe unpressurized high-altitude cases (around −55 °C to +85 °C, up to roughly 21,300 m / 70,000 ft), and the section also addresses decompression and overpressure. Because it is part of the civil airworthiness path, the category you qualify against is tied to where the equipment sits in the aircraft.

MIL-STD-810 Method 500.6 (Low Pressure / Altitude)

Method 500.6 defines four procedures: I — Storage, II — Operation, III — Rapid Decompression, and IV — Explosive Decompression. Air-transport conditions are often set at 4,572 m (15,000 ft, 57.2 kPa). Rapid decompression takes the chamber from 2,438 m (8,000 ft, 75.2 kPa) to 12,192 m (40,000 ft, 18.8 kPa) in no more than 15 seconds; explosive decompression performs the same drop in 0.1 second. The method is tailored to the platform's altitude profile and is not intended for equipment flying above 21,300 m (70,000 ft); the test altitude should reflect the maximum the transport mode actually reaches.

Differences — and combining

DO-160 fuses temperature and altitude into one civil-certification test, with categories you comply against. MIL-STD-810 treats low pressure as a tailored method you select per deployment, and for combined climatic-altitude-vibration effects it points to Method 520. The two frameworks share the same physics; the choice follows your certification route. In practice, altitude is most revealing when run together with temperature, as both standards recognize.

Testing with ULMEKA

ULMEKA designs altitude and low-pressure test systems — combined with temperature where the program requires it — under PLC + HMI control with real-time monitoring of pressure and temperature. Whether your requirement is a DO-160 category or MIL-STD-810 Method 500.6, tell us the standard, the procedures and your specimen dimensions, and we will propose a matched system.