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1. |
Estimation and prediction of the heats of formation for non‐aromatic polynitro compounds on the basis of the QSPR approach |
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Propellants, Explosives, Pyrotechnics,
Volume 19,
Issue 4,
1994,
Page 159-164
Dmitrii V. Sukhachev,
Tatyana S. Pivina,
Fred S. Volk,
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摘要:
AbstractThe analysis of “Quantitative Structure‐Property Relationship”(QSPR), concerning the heat of formation in the condensed state, is performed for non‐aromatic polynitrocompounds. The QSPR approach and our original computer program “EMMA”(Efficient Modelling of Molecular Activity) are used. This approach is based on the construction of optimal linear regression models involving physical‐chemical, topological, informational, and substructural indices; it can be used as an alternative to traditional additive schemes for evaluating physical‐chemical characteristics of energetic materials. On the basis of the QSPR method, the “structure‐heat of formation (ΔH°f)” relationship is revealed for a data base of non‐aromatic polynitrocompounds, and ΔH°fis predicted for
ISSN:0721-3115
DOI:10.1002/prep.19940190402
出版商:WILEY‐VCH Verlag GmbH
年代:1994
数据来源: WILEY
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2. |
Ignition mechanism of the Zr/PbCrO4pyrotechnic mixture in presence of an oxidizing atmosphere |
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Propellants, Explosives, Pyrotechnics,
Volume 19,
Issue 4,
1994,
Page 165-170
C. Brassy,
F. Marlin,
M. Roux,
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摘要:
AbstractIn presence of oxygen, the Zr/PbCrO4(60%/40%) solid mixture exhibits a high amplitude exothermal reaction at low temperature (before reaching the oxidant decomposition temperature). We assume that the reaction is entertained by the air oxygen which continuously diffuses into the mixture pores.The solid‐phase diffusion of oxygen through a zircon layer seems to constitute the limiting step of the reaction. To verify this assumption, a model allowing for diffusion in a protective oxide is developed. The results obtained with this model correspond to the tests for an apparent energy diffusion value varying between 130 kJ/mol and 170 kJ/mol. A value of 130 kJ/mol corresponds to the migration energy of the anionic gaps in a porous zircon layer. The evolution of the apparent diffusion energy can be attributed to the formation energy of crystalline defects (in particular anionic gaps
ISSN:0721-3115
DOI:10.1002/prep.19940190403
出版商:WILEY‐VCH Verlag GmbH
年代:1994
数据来源: WILEY
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3. |
Analysis of 2‐Nitrodiphenylamine and its Major Derivatives in double and triple base propellants |
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Propellants, Explosives, Pyrotechnics,
Volume 19,
Issue 4,
1994,
Page 171-173
L. Kansas,
D. Robertson,
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摘要:
AbstractHigh performance liquid chromatography is used to separate 2‐nitrodiphenylamine and its major reaction products with nitrogen oxide in double and triple base rocket and artillery propellants. A reversed phase, isocratic technique is employed. Analysis of samples stored at ambient and elevated temperatures is discusse
ISSN:0721-3115
DOI:10.1002/prep.19940190404
出版商:WILEY‐VCH Verlag GmbH
年代:1994
数据来源: WILEY
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4. |
Synthesis, Properties and Performance of the High Explosive ANTA |
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Propellants, Explosives, Pyrotechnics,
Volume 19,
Issue 4,
1994,
Page 174-179
R. L. Simpson,
P. F. Pagoria,
A. R. Mitchell,
C. L. Coon,
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摘要:
Abstract3‐Amino‐5nitro‐1,2,4‐triazole(ANTA) was prepared and evaluated in terms of insensitivity and performance. The material is very insensitive to impact and moderately so to thermal stimuli. Performance was found to be inferior to 1,3,5‐triamino‐2,4,6‐trinitrobenzene (TATB). The best synthesis of ANTA is a three‐step route using commercially available 3,5‐diami
ISSN:0721-3115
DOI:10.1002/prep.19940190405
出版商:WILEY‐VCH Verlag GmbH
年代:1994
数据来源: WILEY
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5. |
Burning Rate Augmentation of BAMO Based Propellants |
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Propellants, Explosives, Pyrotechnics,
Volume 19,
Issue 4,
1994,
Page 180-186
Yoshio Oyumi,
Kiyotaka Inokami,
Kazuhiro Yamazaki,
Koki Matsumoto,
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摘要:
AbstractThermal decomposition and the burning properties of BAMO based propellants with HMX or AN/HMX have been investigated. The heat generated by the azide binder decomposition initiated and accelerated the thermal decomposition of HMX and AN. Ammonium perchlorate (AP) and lead stearate with carbon black significantly altered the mechanisms of the thermal decomposition and the burning properties of the HMX based propellants. AP showed an increase in burning rate with a slight decrease in burning rate pressure exponent. The lead catalyst yielded high value of the burning rate with the lowest pressure exponent. The ammonium dichromate also influenced the mechanisms of the thermal decomposition and the burning properties of the AN/HMX samples. The combination of ammonium dichromate and copper chromite was the most effective on the burning rate augmentation of AN/HMX based propellants. AN sublimed and evaporated from the condensed phase and mainly reacted exothermically in the gas phase HMX and AN/HMX based propellants showed smokeless burning characteristics in the small rocket motor combustion tests.
ISSN:0721-3115
DOI:10.1002/prep.19940190406
出版商:WILEY‐VCH Verlag GmbH
年代:1994
数据来源: WILEY
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6. |
Testing the Precision Initiation Couplers |
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Propellants, Explosives, Pyrotechnics,
Volume 19,
Issue 4,
1994,
Page 187-191
Manfred Held,
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摘要:
AbstractIt is possible to properly test a Precision Initiation Coupler (PIC) for its detonation profile and the rotational symmetry of its detonation wave using the Multi‐Streak and/or Flash‐Gap‐Technique both with central linear streak line and circle streak which is comprised of dots for better evalu
ISSN:0721-3115
DOI:10.1002/prep.19940190407
出版商:WILEY‐VCH Verlag GmbH
年代:1994
数据来源: WILEY
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7. |
Modified SDM Model for the Calculation of shaped charge hole profiles |
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Propellants, Explosives, Pyrotechnics,
Volume 19,
Issue 4,
1994,
Page 192-201
Wolfgang Schwartz,
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摘要:
AbstractShaped charge craters can be calculated in regards to depth and diameter profile using the SDM model named after Simon, DiPersio, and Merendino(3). Crater profiles calculated using the SDM formulae exhibit a systematic deviation if compared with test data from firings of certain MBB (now DASA) shaped charges into RHA.The calculated craters feature a significantly more trumpet‐shaped profile than the measured holes in RHA This phenomenon is caused, at least partly, by the assumption in the SDM model that the break‐up time and the jet diameter after break‐up are constant. Radiographs of particulated jets provide evidence that the diameter is generally not constant, rather increases from tip to tail. The evaluation of such radiographs also leads to the conclusion of variable break‐up times.Changing those two assumptions a modified set of SDM formulae was developed so that calculated and experimental crater profiles are in better agreement for the above mentioned MBB shaped
ISSN:0721-3115
DOI:10.1002/prep.19940190408
出版商:WILEY‐VCH Verlag GmbH
年代:1994
数据来源: WILEY
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8. |
Flame Atomic Absorption Spectrometric Determination of lead and titanium in samples of double‐base propellants |
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Propellants, Explosives, Pyrotechnics,
Volume 19,
Issue 4,
1994,
Page 202-205
Sadiq J. Baqir,
Fadhil Jasim,
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摘要:
AbstractThis research demonstrates how additives such as Pb(II) and Ti(IV) in powders of double‐base propellants (D‐BP) could be analysed by flame atomic absorption spectrometry (F‐AAS). No separation or preconcentration is needed. Both direct and spiked techniques have been applied successfully. The use of synthetic (simulated) D‐BP calibration standards is advocated for the analysis of real (D‐BP) samples. The effects of diverse ions and matrix modifiers are investigated. Sensitivity, detection limit, linearity, RSD% and recovery percent are calculated. It is foreseen that this analysis is suited to further application in other additives (usually present in D‐BP) e.g., nickel, cobalt, zinc, manganese, calci
ISSN:0721-3115
DOI:10.1002/prep.19940190409
出版商:WILEY‐VCH Verlag GmbH
年代:1994
数据来源: WILEY
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9. |
The Solubility of ϵ‐CL‐20 in Selected Materials |
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Propellants, Explosives, Pyrotechnics,
Volume 19,
Issue 4,
1994,
Page 206-212
Erica von Holtz,
Donald Ornellas,
M. Frances Foltz,
Jack E. Clarkson,
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摘要:
AbstractThe solubility of the epsilon polymorph of CL‐20 was determined in thirteen liquids over the temperature range of ambient to 74°C using high performance liquid chromatography. The experiments included ϵ‐CL‐20 produced by two different synthesis routes; one lot contained a higher level of polymorphic impurity, the other lot contained a higher level of non‐CL‐20 impurity.In general, the ϵ‐CL‐20 was found to be highly soluble in the solvents with carbonyl groups, and relatively insoluble in hydrocarbons and materials containing ether linkages. The amount of phase conversion to γ‐CL‐20 which occured during the solubility testing was measured using FTIR, and ranged from essentially zero to ∼ 10% conversion. It appears that the presence of β‐CL‐20 in the virgin ϵ‐CL‐20 lots will affect the amount of gamma
ISSN:0721-3115
DOI:10.1002/prep.19940190410
出版商:WILEY‐VCH Verlag GmbH
年代:1994
数据来源: WILEY
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10. |
Forthcoming Meetings |
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Propellants, Explosives, Pyrotechnics,
Volume 19,
Issue 4,
1994,
Page 213-214
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ISSN:0721-3115
DOI:10.1002/prep.19940190411
出版商:WILEY‐VCH Verlag GmbH
年代:1994
数据来源: WILEY
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