Combined Temperature and Low-Pressure Testing to 65,000 Feet Simulated Altitude
Aircraft, satellites, and rockets experience a combination of extreme temperature and low atmospheric pressure that a standard temperature chamber can't reproduce. Sonacme's altitude test chambers combine high/low temperature control with low air pressure simulation, testing components and assemblies from ground-level conditions up to 65,000 feet simulated altitude in a single chamber.
Built to meet DEF STAN 00-35 (Parts 3-11 and 3-12, high temperature/low pressure) alongside broader MIL-STD and RTCA low-pressure test requirements, for satellite, rocket, airplane, and helicopter component qualification.
| Model | Altitude Range | Compliance | |
|---|---|---|---|
| Altitude Temperature Chamber | On-site altitude to 65,000 ft | DEF STAN 00-35 3-11/3-12, MIL-STD, RTCA | Enquire |