| Обозначение | Заглавие на русском языке | Статус | Язык документа | Цена (с НДС 20%)
в рублях |
|
|
Specification for plate of aluminium-copper-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for plate of aluminium-zinc-magnesium-copper-chromium alloy (solution treated, controlled stretched and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for ingots and castings of aluminium-silicon-magnesium alloy (solution treated and precipitation treated) (Si 7, Mg 0.3)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for ingots and castings of magnesium-cerium-zinc-zirconium alloy (precipitation treated) (rare earth metals 3.0, Zn 2.3, Zr 0.6)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for ingots and castings of magnesium-zinc-cerium-zirconium alloy (precipitation treated) (Zn 4.5, rare earth metals 1.2, Zr 0.7)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Ingots (as cast) and castings (solution treated and artificially aged) of aluminium-silicon-magnesium alloy (Si 7, Mg 0.6)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Methods of numbering propulsion units and components and describing their direction of rotation
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for outside diameters and thicknesses of tubing
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for retreading of cross ply tyres for aircraft
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Aircraft. Hydraulic components. Marking to indicate fluid for which component is approved
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Aircraft. Fluid systems. Thermal shock testing of piping and fittings
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for aircraft material. 40 carbon steel (normalized) (35/45 tonf/sq in: limiting ruling section 6 in)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification 2 per cent nickel-chromium-molybdenum steel. (1000/1160 MPa: limiting ruling section 150 mm)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for 18/9 chromium-nickel corrosion-resisting steel (titanium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for 18/9 chromium-nickel corrosion-resisting steel (niobium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for high thermal expansion steel billets, bars, forgings and parts (620 MPa: limiting ruling section 150 mm)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for 1% carbon-chromium steel billets, bars, forgings and parts (limiting ruling section 25 mm)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for 1% carbon-chromium steel (vacuum arc remelted) billets, bars, forgings and parts (limiting ruling section 25 mm)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
|
|
Specification for high chromium-nickel corrosion-resisting steel bright bars (free machining) (880-1080 MPa: limiting ruling section 70 mm)
|
|
|
На языке оригинала
|
Пишите на gost@gostinfo.ru
|
|
| Страницы: ... / 231 / 232 / 233 / 234 / 235 / 236 / 237 / 238 / 239 / 240 / 241 / 242 / 243 / 244 ... / 2197 |