Search results
Results from the WOW.Com Content Network
1 Material Safety Data Sheet. 2 Structure and properties. 3 References. Toggle the table of contents. Hydrochloric acid (data page) ... Download QR code; Print/export
These safety phrases were used internationally and not just in Europe, and there is an ongoing effort towards complete international harmonization. This harmonization would be carried out by the United Nations 's Globally Harmonized System of Classification and Labelling of Chemicals , that replaced Directive 67/548/EEC under CLP Regulation .
An example SDS, including guidance for handling a hazardous substance and information on its composition and properties. A safety data sheet (SDS), [1] material safety data sheet (MSDS), or product safety data sheet (PSDS) is a document that lists information relating to occupational safety and health for the use of various substances and products.
Code Phrase R1 Explosive when dry R2 Risk of explosion by shock, friction, fire, or other sources of ignition R3 Extreme risk of explosion by shock, friction, fire, or other sources of ignition R4 Forms very sensitive explosive metallic compounds R5 Heating may cause an explosion R6 Explosive with or without contact with air R7 May cause fire R8
The engine has an overall pressure ratio of 35:1, which is extremely high for an engine with a centrifugal compressor. Other cycle parameters are a bypass ratio of 5.3 and airflow of 240 lb/s (108.9 kg/s).
The -5 model was certified in 1982, and a decade later, an engine utilizing the TFE731-5 power section and a TFE731-3 fan was built and designated the TFE731-4, intended to power the Cessna Citation VII aircraft. [4] The most recent version is the TFE731-50, based on the -60 used on the Falcon 900DX, which underwent its flight test program in ...
While its predecessor, the XF5, was a small engine, the XF9-1 prototype is close to the General Electric F110 in size, and is comparable to the Pratt & Whitney F119 in terms of thrust class. With the core that withstands 2,073 K (1,800°C) class Turbine Inlet Temperature, [ 4 ] the XF9-1 produces a high thrust, improving fuel economy at the ...
The 2,500 lbf (11 kN) thrust PW625F demonstrator engine was first run on 31 October 2001. [1] It flew in late 2002. [2] In 2002, the PW610F was selected for the Eclipse 500 twinjet, replacing the EJ22 as Williams was unable to reach sufficient reliability. The 950 lbf (4.2 kN) thrust engine was certified by Transport Canada on 27 July 2006. [3]