Hydrocarbon Safety Chamber (MIL-DO-160)
Climats
Secure hot-cold chamber for kerosene-filled aviation fuel tank testing, -70°C to +180°C, per MIL-DO-160.
Technical specifications
- Temperature Range
- -70°C to +180°C
- Speed Variation
- 10°C/min average from +70°C to -55°C (30kg load, 1kW dissipation)
- Standard
- MIL-DO 160 military and civil aeronautical standard
- Useful Dimensions (W×D×H)
- 1000 × 1000 × 1000 mm
About
Secure Hot-Cold chamber to carry out tests with tanks filled up with kerosene. The chamber aims to characterize the tank and all its sub-assemblies: kerosene supply circuit, temperature, pressure, valves. These tanks are used in both civil and military aviation, including helicopters. Features include low-load resistors, fluorinated silicone seals, skin temperature measurement of electrical resistors, nitrogen inerting with high and low flow rates, door opening safety device, and oxygen concentration sampling. Designed to comply with the MIL-DO 160 military and civil aeronautical standard.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.