Density @ 15ºC, kg/m3 775 to 840 775.0 to 840.0 Freeze Point, ºC -40 Max -47.0 Max Viscosity @ -20ºC, mm/s 8.0 Max. 8.000 Max. Net Heat of Combustion, MJ/kg 42.8 Min. 42.80 Min. One of the following shall be met: ...
Density at 15 oC Kg per L 0.775 min. GB/T1884 GB/T1885 Viscosity at -20 oC Mm2 per Sec. 8 max. GB/T265 GB/T11137 Smoke point Mm 25 min. GB/T382 Percentage naphthalene Vol. % 3 max. Net calorific value Mega joul per Kg 42.8 min. GB/T384 GB/T2429 Coper corrosion (2 hrs...
1218D86 lnitialboilingpoint Fuelrecovered Report 10﹪vol.,at℃ Max.205.0 50﹪vol.,at℃ Report 90﹪vol.,at℃ Report Finalboilingpoint,℃ Max.300.0 Residue,﹪Vol. Max.1.5 Loss,﹪Vol. Max.1.5 閃點:Flashpoint,℃ Min.40(大林廠)14473 13429 D3828 D56(註8) 密度:Densityat15℃,Kg/L Min. ...
内容提示: 航空燃油 JET A-1 規範 版別:2.7 頁次:1/4 Specifications for Aviation Turbine JET A-1(註 1) 產品編號:Products No. 外觀(Appearance): 視 目(Visual)Jet A-1 113-F31001 於常溫下清澈 , 無固體物質及水份 (Clear 、bright and visually free from solid matter and un-dissolved water ...
A composite liner comprised of a fluorinated high-density polyethylene (f-HDPE) geomembrane and geosynthetic clay liner (GCL) was used to contain a hydrocarbon spill in the Canadian Arctic. Results of laboratory tests conducted to assess the effect of exposure to cold climates and hydrocarbons on ...
Densityat15oCKgperL0.775min.GB/T1884 GB/T1885 Viscosityat-20oCMm2perSec.8max.GB/T265 GB/T11137 SmokepointMm25min.GB/T382 Percentage naphthalene Vol.%3max. NetcalorificvalueMegajoulperKg42.8min.GB/T384GB/T2429 Copercorrosion(2hrs. at100oC) Classification1maxGB/T5096 Thermalstabilityat260 ...
High-density discharges on JET with ITER-like Wall (ILW) have been analysed with the aim of establishing a mechanism for the H-mode density limit (DL) and compared with experiments in the JET carbon material configuration. The density limit is up to 20% higher in the JET-ILW than in ...
Jet A-1 fuel and RME (B100) blends properties are indirect between Jet A-1 and RME properties. The density, kinematic viscosity at 40C, cloud point (CP), cold filter plugging point (CFPP) and pour point (PP) RME, B100, Jet A-1 and their blends were measured. Adding the Jet A-1...
Type:Jet A-1;D2 or Not:Is D2;Place of Origin:KZ;Density:210 centigrade;Flash Point:38centigrade;Freezing Point:-47centigrade;Brand Name:Jet A-1;Model Number:002;|Alibaba.com
The high energy density of the rocket provides a 100-fold increase in thrust over air-breathing engines of similar size. 1.3 Chemical Rocket Requirements The energy requirements of a rocket are typically stated in terms of velocity increment or ΔV. The flight velocity required to escape from ...