用微量热法测定稀土含硫有机配合物的比热容

推导了用改进的RD496-III型微热量计测定固态物质比热容的计算式. 用Joule 效应确定了仪器在298.15 K时的量热常数和相对标准偏差分别为(63.901±0.030) μV•mW^－1和0.08%, 用Peltier效应测定总不平衡热. 在该仪器上测定的两种标准物质(基准苯甲酸和α-Al₂O₃)比热容的计算值与文献值相差在0.4%以内. 用本法测定了13种固态配合物RE(PDC)₃(phen) (RE＝La, Pr, Nd, Sm～Lu; PDC＝ )的比热容值, 总偏差在1.0%, 与稀土原子序数Z_RE作图呈现“三分组现象”, 说明配合物中RE^3＋与配体间的化学键有一定程度的共价性, 显示了稀土离子4f电子云的扩大效应.     

Thermochemical Properties and Non-isothermal Decomposition Reaction Kinetics of N-Guanylurea Dinitramide （GUDN）

Introduction N-Guanylurea dinitramide (GUDN) is a new ener-getic oxidizer with higher energy and lower sensitivity. Its crystal density is 1.755 g·cm-3. The detonation velocity is about 8210 m·s-1. Its specific impulse and pressure exponent are 213.1 s and 0.73, respectively. It has the potential for possible use as an energy ingredient of propellants and explosives from the point of view of the above-mentioned high performance. Its preparation,1 properties2 and hygroscopocity2 have been …     

Thermochemistry of the Ternary Complex Nd（Et2dtc）3（phen）

Introduction A series of lanthanide sulfide complexes have beenlargely used for ceramics and thin film materials1 andthese complexes could be prepared from the precursorswhich are the compounds containing lanthanide-sulfurbonds.2-4 For instance, the compounds synthesized with[(alkyl)2dtc]-, phen?H2O and lanthanide salts were usedas the volatile precursors for preparing lanthanide sul-fide, its friction properties in lubricant was investigatedin literature 5 and the preparation and propertie…     

Thermal Decomposition Behavior and Non-isothermal Decom-position Reaction of Copper(II) Salt of 4-Hydroxy-3,5-dinitro- pyridine Oxide and Its Application in Solid Rocket Propellant

Introduction Copper(II) salt of 4-hydroxy-3,5-dinitropyridine ox-ide (4HDNPOCu) is an energetic material containing energetic groups of NO2, which can be used as an ener-getic auxiliary catalyst substituting the inertia copper salt to improve the catalysis of the main catalyst (lead salt) in Composite Modified Double Base propellant containing RDX (RDX-CMDB propellant).1 Thermal behavior is one of the most important aspects affecting its catalytic efficiency for propellant. However, …