Country Of Origin - HP Elite x2 1012 G1 Quickspecs

QuickSpecs
Technical Specifications
Dust*
Vibration*
Vibration 2*
Shock*
Freeze/Thaw test*
Sand test*
Explosive Atmosphere*
*MIL STD 810G testing is not intended to demonstrate fitness for U.S. Department of Defense contract requirements or for
military use. Test results are not a guarantee of future performance under these test conditions. Damage under the MIL STD test
conditions or any accidental damage requires an optional HP Accidental Damage Protection Care Pack.

COUNTRY OF ORIGIN

China
Not all configuration components are available in all regions/countries.
c04895999 — DA – 15477 — Worldwide — Version 16 – March 22, 2017
3ft onto every side, angle and edge onto 2" of plywood over
steel over concrete.
The dust test was performed in accordance with MIL-STD-810G,
Method 510.5, Procedure I. Test parameters were set so that the
unit was dusted with Arizona Road Dust for six hours while being
operated. Each cycle was one day (24 hours); ten cycles with the
temperature being cycled between 30°C (86°F) and 60°C (140°F);
and relative humidity was a constant 95%.
The vibration test was performed in accordance with MIL-STD-
810G, Method 514.6, Procedure I category 4. This test evaluated
the units performance after it has been subjected to higher
levels of vibration while in storage: Operational U.S. highway
truck exposure, 1000 mile Simulation and One hour/axis
duration.
The vibration test was performed in accordance with MIL-STD-
810G, Method 514.6, Procedure I category 24. This test
evaluated the units performance after it has been subjected to
higher levels of vibration while in storage: Non-operational 0.04
g2/Hz at 20-1000 Hz, -6 dB/octave at 1000-2000 Hz and One
hour/axis duration.
The shock test was performed in accordance with IL-STD-810G,
Method 516.6.5, Procedure I. This test objective was to
determine whether the unit could be safely operated after being
exposed to sudden physical shock events while operational. For
this test, 3 shocks were performed across each axis and
direction for a total of 18 shocks -40Gs peak, 11ms.
The Freeze/Thaw test was performed in accordance with MIL-
STD-810G, Method 524.54 Procedure III. The objective of
this test was to determine whether the unit could be safely
operated after being exposed to a temperature drop of -10°C
(14°F) for two hours. Unit is removed and checked for operation.
The Sand test was performed in accordance with MIL-STD-810G,
Method 510.5 Procedure II
The Explosive Atmosphere test was performed in accordance
with MIL-STD 810G, Method 511.5 Procedure I.
HP Elite x2 1012 G1
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