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Vacuum Stability Test

Vacuum stability testing for propellant powders and explosives per MIL-STD-286C and STANAG 4556.

MIL-STD-286CSTANAG 4556
Vacuum Stability Test
Bores 15 × Ø 15,75 mm, Tiefe 125 mm
Control accuracy ±0,1 °C
Max. temperature 135 °C

Description

Device for determining the thermal stability of nitrocellulose and other nitro compounds, single- and double-base propellants per MIL-STD-286C Method 403.1.3 and STANAG 4556, Procedure 1, Vacuum Stability Test (with manometric method).

Scope of delivery

  • Heavy aluminum heating block (15 bores Ø 15.75 mm, depth 125 mm), PT100 sensor, over-temperature protection (150 °C)
  • Programmable PID controller in a separate control box (control accuracy ±0.1 °C, max. 135 °C)
  • 15 test tubes with mercury collar, capillary tubes with mercury cup (Ø 15 mm × 155 mm)
  • Rack for filling the glass unit with mercury
  • Vacuum pump IP44: 4-stage diaphragm pump, max. vacuum 0.6 mbar, max. suction capacity 13 l/min
  • Heavy aluminum heating block with 15 bores
  • Programmable PID control (±0.1 °C)
  • Vacuum pump IP44 (4-stage, max. 0.6 mbar)
  • Manometric method per STANAG 4556

Technical data

Bores 15 × Ø 15,75 mm, Tiefe 125 mm
Control accuracy ±0,1 °C
Max. temperature 135 °C
Power 1.800 VA
Mains voltage 230 V / 50 – 60 Hz
Cable length ca. 2 m
Vacuum pump 4-stage, max. 0,6 mbar, 13 l/min

Standards & Norms

MIL-STD-286CSTANAG 4556

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