• Inertial navigation test table with 600mm diameter stainless platform and integrated thermal control
  • Close up of precision bearing system for better than 0.5 arcsec angular repeatability
  • Rate table performing -55 degree low temperature cycle for aircraft INS calibration
  • Test equipment dimensions with 600mm table diameter on reinforced aerospace workbench
  • Remote automated interface executing thermal profile for military navigation system testing
  • Inertial navigation test table with 600mm diameter stainless platform and integrated thermal control
  • Close up of precision bearing system for better than 0.5 arcsec angular repeatability
  • Rate table performing -55 degree low temperature cycle for aircraft INS calibration
  • Test equipment dimensions with 600mm table diameter on reinforced aerospace workbench
  • Remote automated interface executing thermal profile for military navigation system testing

Heavy Duty Dual Axis Rate Table with Thermal Chamber for Aircraft Navigation Testing

No.BE-INS2-DT23V
This heavy duty dual axis rate table serves as inertial navigation test table and gyro calibration fixture for aircraft navigation systems under extreme temperatures. 80kg payload capacity accommodates large avionics assemblies, built-in thermal chamber from -55℃ to +85℃ simulates harsh flight environments, and better than 0.5″ angular repeatability ensures precise gyro validation. Ideal for aircraft INS testing, navigation system calibration, and satellite component temperature cycling.
Specifications
Load weight:
80kg
Working desk:
600mm
Table surface flatness:
0.008mm
Table runout:
0.01mm
Temperature range:
≥ -55°C ~ 85°C
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  • Inertial navigation test table with 600mm diameter stainless platform and integrated thermal control
  • Close up of precision bearing system for better than 0.5 arcsec angular repeatability
  • Rate table performing -55 degree low temperature cycle for aircraft INS calibration
  • Test equipment dimensions with 600mm table diameter on reinforced aerospace workbench
  • Remote automated interface executing thermal profile for military navigation system testing

Description

No. Indicator Item Technical Parameters
1 Load weight 80kg
2 Working desk 600mm
3 Table surface flatness 0.008mm
4 Table runout 0.01mm
5 Verticality (table and spindle) No more than ±1.8"
6 Perpendicularity between two axes No more than ±1.8"
7 Box size Not less than 650mm × 650mm × 650mm
8 Temperature range ≥ -55°C ~ 85°C
9 Temperature control accuracy ≤ 0.1°C
10 Temperature uniformity in the chamber ≤ 1°C
11 Temperature control box heating and cooling rate range The temperature control box temperature change rate covers 0.3°C/min ~ 5°C/min and can be set arbitrarily. It is linearly adjustable from 0.3°C/min to 2°C/min within the temperature range of -55°C ~ 85°C.
12 Corner range Both frames are continuous and infinite
13 Angular position measurement resolution Both frames are better than 0.036"
14 Angular position positioning accuracy Inner frame: better than ±1"
Outer frame: better than ±2"
15 Angular position zero return accuracy Inner frame: better than ±1"
Outer frame: better than ±2"
16 Angular position repeatability Both frames are better than 0.5"
17 Rate range Inner frame: ±0.0005°/s ~ ±1000°/s (20kg load)
Inner frame: ±0.0005°/s ~ ±400°/s (40kg load)
Inner frame: ±0.0005°/s ~ ±200°/s (80kg load)
Outer frame: ±0.0005°/s ~ ±200°/s
18 Angular acceleration range Inner frame: ≥ 300°/s²
Outer frame: ≥ 110°/s²
19 Speed resolution Better than 1×10⁻⁶
20 Rate accuracy and stability ±0.0001°/S ~ ±1°/S, Better than 2×10³ (1° average)
±1°/S ~ ±10°/S, Better than 1×10⁴ (10° average)
greater or equal to 10°/S, Better than 1×10⁵ (360° average)