HP Elite x2 1012 G1 Quickspecs page 31

QuickSpecs
Technical Specifications
MIL-STD 810G TEST
High Temperature test*
High Temperature test*
Low Temperature test*
Low Temperature test*
Thermal Shock test*
Altitude*
Humidity*
Drop*
Battery recharge time System in OFF or Standby
Fuel Gauge LED
Optional travel
battery available
Not all configuration components are available in all regions/countries.
c04895999 — DA – 15477 — Worldwide — Version 16 – March 22, 2017
Non-operating
Mode <3 hours
No
No
The High Temperature test was performed in accordance with
MIL-STD-810G, Method 501.5, Procedure I (Storage). This test
evaluated the units' performance while it was being exposed to
high temperature conditions: 71°C (160°F) nonoperational. Test
cycle 24 hours; test consisted of seven cycles.
The High Temperature test was performed in accordance with
MIL-STD-810G, Method 501.5, Procedure II (Operation). This test
evaluated the units' performance while it was being exposed to
high temperature conditions: 60°C (140°F) operational. Four
hours duration.
The Low Temperature test was performed in accordance with
MIL-STD-810G, Method 502.5, Procedure I (Storage). This test
evaluated the unit's performance while it was being exposed to
low temperature conditions: -51°C (-60°F) nonoperational. Four
hours duration.
The Low Temperature test was performed in accordance with
MIL-STD-810G, Method 502.5, Procedure II (Operation). This test
evaluated the unit's performance while it was being exposed to
low temperature conditions: -29°C (20°F) operational. Four hour
duration.
The Thermal Shock test was performed in accordance with MIL-
STD-810G, Method 503.5, Procedure I. The objective of this test
was to determine whether the unit could be safely operated
after being exposed to sudden changes in ambient
temperature while non-operational. The high temperature was
set to be 96°C (205°F) and the low temperature to be
-51°C (-60°F); three high-to-low cycles were performed.
The Altitude test was performed in accordance with MIL-STD-
810G, Method 500.5, Procedure I (Storage) and II (Operation).
The altitude level simulated for both procedures was 15,000
feet at 57kPa.Four hour duration.
The humidity test was performed in accordance with MIL-STD-
810G, Method 507.5, Procedure II. Relative humidity 95%.
Temperature cycled between 86oF and 140oF.Test cycle 24
hours; test consisted of ten cycles.
The drop test was performed in accordance with MIL-STD-810G,
Method 516.6, Procedure IV. The objective of this test was to
determine whether the unit was operational after being dropped
from desk height. For this test, 26 drops were performed from
HP Elite x2 1012 G1
-4° to 140° F ( -20° to 60° C )
Page 31