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71.
本法采用新型硝化剂HNO3-P2O5-NH4NO3硝解DPT制备HMX,并用日立635型高效液相色谱肖解混合物HMX/RDX中的HMX含量,测定HMX得率。实验结果表明:本法制得的HMX得率大于60%,已接近用醋酐法由DPT制备HMX的得率,这是非醋酐法制备HMX取得的新进展。 相似文献
72.
Yi Wang Xiaolan Song Dan Song Wei Jiang Hongying Liu Fengsheng Li 《Propellants, Explosives, Pyrotechnics》2011,36(6):505-512
Three fabrication methods were used to synthesize HMX powders with different particle sizes and microscopic morphologies. All as‐prepared samples were characterized by laser granularity measurements and scanning electron microscopy (SEM). The mechanical sensitivity and thermal stability of the different HMX powders were characterized using mechanical sensitivity tests and differential scanning calorimetry (DSC). Size distribution data and SEM images were used to find the size fractal dimension (D) and surface fractal dimension (Ds) of HMX samples, which were calculated by the least‐squares method and fractal image processing software (FIPS), respectively. The parameters D and Ds quantize two important properties of HMX particles, namely the complexity of the particle size distribution and the irregularity of the particle surface, which affect the thermal conductivity of the particle group if it is exposed to stimuli such as impact, friction or heating. The fractal dimensions reveal the dependence of the mechanical sensitivity of HMX on the powder size, size distribution and microscopic morphology. The results indicate that the proportion of fine particles in HMX powder increases as the D value increases, which causes decreased impact sensitivity. This occurs because hot spot formation leading to an explosion is more difficult because of the improved thermal conductivity of the particle group. Similarly, the surface roughness of HMX particles increases with an increase in Ds, causing an increase in friction sensitivity because of the excessive accumulation of frictional heat. In addition, thermal analysis results indicate that the maximum thermal decomposition rate of HMX decreases with increasing D and Ds. 相似文献
73.
为研究还原型锡酸铅粒度对Al/HMX/CMDB推进剂燃烧性能及安定性的影响,采用干筛法筛选6种不同粒度的还原型锡酸铅,制备了含不同粒度还原型锡酸铅体系的推进剂;通过燃速靶线试验、甲基紫试验与热加速老化试验得到推进剂的燃速、压强指数、甲基紫变色时间和贮存寿命。结果表明,随还原型锡酸铅粒径由7.0μm减至2.5μm,Pb2+及SnO2的催化活性逐渐增大,活化中心愈多,该体系推进剂在15~20MPa范围内的燃速逐渐增加,压强指数由0.30减至0.17;同时还原型锡酸铅粒度的减小加速了该体系推进剂的自催化作用,造成其安定性下降,当还原型锡酸铅的粒径为2.5~3.5μm时,推进剂的安定性显著降低。 相似文献
74.
Explosive characteristics of aluminized HMX-based nanocomposites 总被引:1,自引:0,他引:1
M. F. Gogulya M. N. Makhov M. A. Brazhnikov A. Yu. Dolgoborodov V. I. Arkhipov A. N. Zhigach I. O. Leipunskii M. L. Kuskov 《Combustion, Explosion, and Shock Waves》2008,44(2):198-212
The explosive characteristics of HMX compositions doped with 15% Al (by weight) were studied experimentally. The detonation
velocity, pressure and temperature profiles, the velocity of endwise acceleration of plates, and the heat of explosion of
dense pressed samples were measured. The results were compared for compositions based on mechanical mixtures of initial micron-size
particles of HMX with aluminum powders of various sizes and for nanocomposites. The addition of nanoaluminum reduces the detonation
velocity to a greater degree than the addition of micron-size aluminum. The mechanical mixtures have close detonation velocities,
whereas in composites containing different types of nanoaluminum, they differ by almost 200 m/sec. For all compositions, except
for the most homogeneous nanocomposite, two-peak pressure profiles are observed. For charges of a composite and a mechanical
mixture with nanoaluminum of the same type, the second peak pressures almost coincide but are reached in different times.
At the same time, the peak pressure increases with decreasing aluminum particle size. The temperature profiles agree qualitatively
with the pressure profiles. The velocity of endwise acceleration of plates depends linearly on the activity of the aluminum
powder used. Nanocomposites and mechanical mixtures containing the same aluminum powder have close heats of explosion. Nanoaluminum
is almost completely oxidized during calorimeter bomb tests, and the major factor determining the heat of explosion of the
compositions with nanoaluminum is also the content of active metal in the aluminum powder.
__________
Translated from Fizika Goreniya i Vzryva, Vol. 44, No. 2, pp. 85–100, March–April, 2008. 相似文献
75.
Chunxue Wei Hui Huang Xiaohui Duan Chonghua Pei 《Propellants, Explosives, Pyrotechnics》2011,36(5):416-423
In this study, a new co‐crystal explosive of 1,3,5,7‐tetranitro‐1,3,5,7‐tetrazocane (HMX)/1,3,5‐triamino‐2,4,6‐trinitrobenzene (TATB) (molar ratio 1 : 1) was designed based on crystal engineering. The crystal structure was predicted using the polymorph predictor (PP) method. The main properties of co‐crystal consisting of mechanical properties, stability, and interaction formats were simulated through molecular dynamics methods. Simulated results indicate that the crystal structure of the HMX/TATB co‐crystal may belong to the P , P212121 or P21/c space group. The calculations of the binding energy and the analysis for radial distribution function show that the two components are connected through electrostatic hydrogen bonding and strong van der Waals interactions. The new co‐crystal has better mechanical properties with the moduli systematically decreased. With the appearance of the new crystal, the trigger bond N NO2 has little change. 相似文献
76.
77.
78.
《Propellants, Explosives, Pyrotechnics》2017,42(4):381-385
Composite rocket propellants prepared from nitramine fillers (RDX or HMX), glycidyl azide polymer (GAP) binder and energetic plasticizers are potential substitutes for smokeless double‐base propellants in some rocket motors. In this work, we report GAP‐RDX propellants, wherein the nitramine filler has been partly or wholly replaced by 1,1‐diamino‐2,2‐dinitroethylene (FOX‐7). These smokeless propellants, containing 60% energetic solids and 15% N‐butyl‐2‐nitratoethylnitramine (BuNENA) energetic plasticizer, exhibited markedly reduced shock sensitivity with increasing content of FOX‐7. Conversely, addition of FOX‐7 reduced the thermochemical performance of the propellants, and samples without nitramine underwent unsteady combustion at lower pressures (no burn rate catalyst was added). The mechanical characteristics were quite modest for all propellant samples, and binder‐filler interactions improved slightly with increasing content of FOX‐7. Overall, FOX‐7 remains an attractive, but less than ideal, substitute for nitramines in smokeless GAP propellants. 相似文献
79.
80.