Aerospace. Linear hydraulic utility actuator. General specifications1 Scope This document establishes the general requirements for a linear hydraulic utility actuator, herein referred to as a "utility actuator", for use in flight vehicle hydraulic systems at pressures up to 35 000 kPa (5 000 psi). These requirements include: design requirements; test requirements. This document is intended to be used in conjunction with the detail specification that is particular to each application. NOTE Although Brake pistons and

This Technical Report describes the key properties of fast pyrolysis bio-oils and their importance to the fuel quality for use in stationary internal combustion engines

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The Messaging service is a UPnP service that allows control points to use the messaging features provided by a Telephony Server (TS) or a Telephony Client (TC)

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The method does not measure fluorocarbons

Addition of requirements for means of access

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distribution power systems were not originally designed to handle these dispersed sources of generation

ISO 22910 can extend its use from AM Ti-alloys to other AM alloys

BS 7851 discusses bibliographical references

BS EN 13179-1:2013 includes some technical changes with respect to EN 13179-1:2000