Next Article in Journal
Major Depressive Disorder and Oxidative Stress: In Silico Investigation of Fluoxetine Activity against ROS
Previous Article in Journal
The Prevention and Control Mechanism of Rockburst Hazards and Its Application in the Construction of a Deeply Buried Tunnel
 
 
Font Type:
Arial Georgia Verdana
Font Size:
Aa Aa Aa
Line Spacing:
Column Width:
Background:
Article

Thermal Analysis and Stability of Boron/Potassium Nitrate Pyrotechnic Composition at 180 °C

1
State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081, China
2
Beijing Space Vehicle General Design Department, China Academy of Space Technology, Beijing 100094, China
3
Safety Technology Research Institute of Ordnance Industry, Beijing 100053, China
4
R & D Center, Liaoning North Huafeng Special Chemistry Co. Ltd., Fushun 113003, China
*
Author to whom correspondence should be addressed.
Submission received: 4 August 2019 / Revised: 27 August 2019 / Accepted: 29 August 2019 / Published: 3 September 2019
(This article belongs to the Section Chemical and Molecular Sciences)

Abstract

:

Featured Application

This research aims to obtain the decomposition process of boron/potassium nitrate pyrotechnic composition, and verify its high temperature stability to meet the charge requirements of the separation device such as the cutter for the lunar probe.

Abstract

Aerospace missions require that pyrotechnic compositions are able to withstand 180 °C. Therefore, this paper studies the thermal stability and output performance of boron/potassium nitrate (abbreviated BPN) used in pyrotechnic devices. Firstly, differential scanning calorimetry (DSC) and thermogravimetric (TG) tests are used to analyze the thermal reaction process of KNO3, boron, and BPN to qualitatively judge their thermal stability. Then, apparent morphology analysis, component analysis, and the p-t curve test, which is the closed bomb test to measure the output power of the pyrotechnic composition, are carried out with BPN samples before and after the high-temperature test to verify BPN stability at 180 °C. The weight change of boron powder caused by chemical reactions occurs above 500 °C. When the temperature is lower than the peak exothermic temperature of decomposition, no obvious chemical reaction occurs with KNO3, and only physical changes (crystal transformation and melting) occur. Combined with a verification test at 180 °C for two days, it is concluded that boron and KNO3 components are stable at 180 °C. With an increase in boron content, the thermal stability of BPN is improved, with the best performance achieved when the ratio is 25:75 (B:KNO3). BPN samples without binder have the best thermal stability. In a test at 180 °C for five days, the binder affects the weight loss and p-t curve of BPN, and BPN with fluororubber binder is better than BPN with unsaturated polyester binder.

1. Introduction

Boron/potassium nitrate (B/KNO3; abbreviated BPN) can be used for the output charge of an engine igniter, a fire transfer charge, a small thrust dynamite output charge, a high temperature projectile charge, etc. BPN has the significant characteristics of high combustion heat and low moisture absorption per unit weight. [1] BPN is also listed as a linear reference for the security of pyrotechnic agents [2].
At present, aerospace missions require that BPN composition is thermally stable. In some special launch missions [3], such as of deep space spacecraft, pyrotechnic devices must withstand a large temperature range, usually from −100 to +130 °C [4,5]. Considering that there is a certain safety margin for temperature, it is of great significance to test and evaluate the thermal stability and output performance of BPN after exposure to the temperature of 180°C, providing a basis for its application in the aerospace field. This research aims to obtain the decomposition process of boron/potassium nitrate pyrotechnic composition, and verify its high temperature stability to meet the charge requirements of the separation device such as the cutter for the lunar probe.
K.R. Rani Krishnan et al. studied the effect on the ignition behavior of potassium boron nitrate pyrotechnic powder of adding RDX and HMX components which are two commonly used high energy explosives. In their paper, thermogravimetric (TG) and differential scanning calorimetry (DSC) analyses which use Perkin Elmer TGA 7 and DSC 7 in flowing argon medium (30 mL min) at 5 °C/min, were carried out on the mixture of potassium boron nitrate and explosive components [6], which provided some inspiration for the present paper. R. Turcotte et al. researched the thermal analysis of black gunpowder in which KNO3 had a pre-ignition reaction under the action of sulfur and charcoal. The pre-ignition reaction occurred at a lower temperature than the decomposition temperature of KNO3 itself, and the decomposition temperature of KNO3 drifted under a complex system [7,8]. ES. Freeman, Seyed Ghorban Hosseini et al. [9,10] studied the thermal decomposition process of KNO3 by the TG-TDA method, and obtained the transformation, melting and decomposition process of KNO3. A. Eslami et al. [11] studied the thermal reaction characteristics of B+KNO3, B+Ba(NO3)2, B+PbO2 and other mixed systems, and the reaction process of a B+KNO3 mixed system was analyzed in stages.
The stability of chemical agents refers to the ability of a sample to maintain its physical, chemical and explosive properties from changing beyond the permitted range under certain circumstances [12]. Stability analysis of physical properties mainly encompasses apparent morphology, color, weight, crystal shape, phase change (melting point, boiling point, volatilization), moisture absorption, particle size, charge density, crystal crack, volatilization, oil permeability, migration, and dielectric constant. Chemical stability encompasses purity, composition, valence state, oxidation state, slow/rapid thermal decomposition, weight loss, and composition of explosive products. The stability of explosion performance encompasses explosion point, detonation heat, detonation velocity, combustion velocity, p-t curve (which is the closed bomb test to measure the output power of the pyrotechnic composition), detonation pressure, detonation capacity, flame sensitivity, hot wire sensitivity, impact sensitivity, friction sensitivity, static inductance, initiation sensitivity, and shock wave sensitivity. In addition to stability, compatibility is also a consideration. This is particularly true of chemical compatibility, including the internal compatibility between the pyrotechnic charge and contact metal (bridge wire, tube shell, cover sheet, motion mechanism, etc.).
At present, there are few reports on the thermal reaction process and high temperature stability. Existing studies of BPN mainly focus on the influence of the preparation process [13,14], particle size [15], ratio [16] and other factors related to ignition performance.

2. Materials and Methods

2.1. Materials

Laboratory reagent grade boron and KNO3 powder were all purchased for tests. The particle size of powdered boron was approximately 1 μm, and KNO3 was 99.5% pure. As shown in Table 1, using boron powder and KNO3 as raw materials, BPN samples with different proportions were prepared.

2.2. Methods

The thermal stability of BPN after exposure at 180 °C was studied by methods such as thermogravimetric analysis and differential scanning calorimetry, and analysis of appearance morphology, weight loss, content, and output performance. The process scheme is shown in Figure 1.
TG and DSC test data were applied to analyze the thermal reaction process of KNO3, boron powder and BPN with different ratios, to qualitatively judge high-temperature stability. The apparent morphology analysis, thermogravimetric (TG) analysis, differential scanning calorimetry (DSC) analysis, and output power test were carried out on BPN samples after the high-temperature test to verify the stability of BPN under a high temperature of 180 °C, thereby providing a basis for its application in the aerospace field. A summary of the analysis method is presented in Table 2.

3. Results and Discussion

3.1. Thermal Analysis of Single Component

The TG process of boron was studied with a nitrogen atmosphere. As shown in Figure 2, a weight loss of approximately 3.3% is observed from heating to 117.5 °C, which reflects the loss of moisture and volatiles in boron powder. Until 500 °C, the quality of boron powder samples increases gradually, and the speed increases after 650 °C. The total mass increases to approximately 118% at 1000 °C. It is speculated that the reaction in this stage is the slow reaction of boron powder and nitrogen, and the final product is BN. The reaction equation is
2B + N2 = 2BN,
The DSC curve of KNO3 has two endothermic peaks. The first endothermic peak (peak temperature 132.6 °C) corresponds to the conversion temperature of KNO3, which is the phase transition of KNO3 from rhombic to trigonal. The second endothermic peak (peak temperature 332.0 °C) corresponds to the melting point of KNO3. [9] The DSC curve shows that the decomposition of KNO3 occurs at more than 500 °C. Combined with the TG curve, the mass change of KNO3 is 5.1% at 545 °C, indicating that KNO3 is melting but is not decomposed or gasified from the melting point (332.0 °C) to the temperature of 500 °C. Therefore, the physical stability of KNO3 changes within the temperature range of 332–500 °C, but the chemical stability is not affected.
A weight loss of KNO3 of 88.1% mainly occurred between 545 °C and 765 °C. According to E.S. Freeman [17], the decomposition of KNO3 took place at this stage, generating nitrite, followed by the decomposition reaction of potassium nitrite, and the product K2O was reported to evaporate (m.p. 380 °C) [10]. The equation of weightlessness in this stage is [8]
2 KNO 3 2 KNO 2 + O 2 ,
4 KNO 2 2 K 2 O + 4 NO + O 2 ,
Compared with the operating condition of 180 °C, the melting temperature of KNO3 at 336.5 °C is about 156 °C higher. No obvious chemical reaction occurs before the peak temperature of decomposition (i.e., more than 545 °C). It can be qualitatively concluded that the boron powder and KNO3 components are stable at a high temperature of 180 °C. It should be noted that this result is obtained according to the reaction temperature of DSC, and the stability of samples at constant temperature needs to be verified.

3.2. Thermal Analysis of BPN with Different Ratios

TG-DSC analysis of BPN samples with different ratios (heating rate 5 °C/min) were carried out, and the curves are shown in Figure 3. For BPN samples with different ratios, the thermal reaction process is similar to that of KNO3 before 500 °C.
As shown in Figure 3, the first endothermic peak (approx. 134 °C) corresponds to the conversion temperature of KNO3, and the second endothermic peak (approx. 332 °C) corresponds to the melting point of KNO3. Before 500 °C, the mass change of sample 1# and 2# is about 9%, while that of sample 3# is less than 5%. Between 500 °C and 650 °C, there is a drastic decomposition reaction, and the sample weight drops sharply. The temperature of the decomposition reaction is about 200 °C higher than the melting point. The main reaction at this stage is
B + KNO 3 KBO 2 + NO .
The weight ratio results of BPN samples with different proportions at typical temperatures are shown in Table 3. At 200 °C, the mass variation of BPN samples with three ratios are in the range 0.9%–1.7%, and at 500 °C, 5.8%–11.4%. At 650 °C, the 2# (25:75) BPN sample (zero oxygen balance ratio) has the least weight loss. Based on TG analysis of KNO3, the initial reaction temperature of BPN (500 °C) is about 50 °C lower than that of KNO3 (545 °C). However, when comparing the endothermic peak temperature of DSC curves of samples, the exothermic peak temperature showed a trend of rising with the increase of boron content, as shown in Table 4.
The results show that with an increase of boron content, the exothermic peak is advanced, but the thermal stability of BPN samples are improved, with the 2#BPN sample (25:75) showing the best performance. Analysis at 180 °C shows that the DSC decomposition temperature of BPN is above 500 °C, and TG weight loss ranges from 5.8% to 11.4% at 500 °C. It can be qualitatively judged that BPN is stable at 180 °C.

3.3. Thermal Exposure Test at 180 °C and Analysis

After drying at 60 °C for 4 h, the samples of BPN, boron powder and KNO3 were placed in a temperature environment testing instrument for a thermal exposure test. The temperature settings were 180 °C for two and five days. The apparent morphology, DSC parameters, weight loss ratios and output performance of samples before and after the test were compared and analyzed.
Apparent Morphology
The apparent morphologies of KNO3, boron and 4#BPN samples before and after different temperature storage are shown in Figure 4, Figure 5 and Figure 6.
After observing the boron powder, KNO3 and 4#BPN samples before and after high temperature, it is found that the color of the KNO3 sample changes slightly from white to yellow, and the particle size and shape do not change. The particle size, shape and color of boron powder and 4#BPN are not observed to change. In addition, there is no change in appearance quality, such as expansion of fractures, loose pits, shrinkage or melting residue.
DSC test
The DSC curves and DSC parameter comparison of 4#BPN sample are given in Figure 7 and Table 5 respectively.
According to the DSC analysis of the variation of the peak temperature, the temperature difference between the first endothermic peak and the second endothermic peak is very small, comparing the samples at 180 °C for two days, 180 °C for five days, and 60 °C for 4 h; ΔT < 1 °C. The exothermic peak temperature variations of the samples at two days and five days are −6.51 °C and −2.77 °C, respectively, but the failure rates of the agents are 1.01% and 3.26%, respectively. This indicates that the exothermic peak temperature of the sample is advanced, but the energy is not consumed. It can be preliminarily concluded that BPN containing KNO3 and boron powder has good thermal stability at 180 °C for two days and five days.
• Weight loss ratio
The weight loss ratios of BPN samples in 180 °C test are given in Table 6. Furthermore, the component variation of BPN samples within 180 °C test are given in Table 7.
As shown in Table 6, from the comparison of the weight loss ratios of BPN samples in the 180 °C test for different times, after five days, the weight loss ratio of 1# BPN without binder is approximately 0.1%, that of 4#BPN containing fluororubber binder is approximately 1%, and that of 5# BPN containing unsaturated polyester is approximately 2%. Combined with the analysis of component content, the change of KNO3 and boron in 1#BPN without binder in the 5-day 180 °C test is 0.5%, i.e., almost no change. Thus, it can be judged to some extent that the stability of BPN in which the main components are KNO3 and boron is well under 180 °C for two days and five days. The reason for the component variation of 4#BPN and 5#BPN is the binder (i.e., 4#BPN contains 3% fluororubber and 5#BPN contains 5.6% unsaturated polyester).
• P-t curve
P-t curve data of BPN samples in 180 °C test is given in Table 8.
It can be seen from the data in Table 8 that the peak pressure of the three kinds of BPN decreases with increasing time of the 180 °C temperature test. The thermal analysis of the single component shows that boron and KNO3 are relatively stable at 180 °C, and the peak pressure attenuation of the 1#BPN sample without binder is 0.95% (i.e., <1%), which also supports this argument. It is also known that the binder has a great impact on the high temperature stability of BPN. The high temperature stability of the fluororubber binder is better than that of unsaturated polyester.

4. Conclusions

In conclusion, we studied the thermal decomposition process of KNO3, boron and BPN based on TG and DSC test data. The weight change of boron powder caused by chemical reaction occurred above 500 °C. When the temperature was lower than the peak exothermic temperature of decomposition, no obvious chemical reaction occurred with KNO3, and only physical changes (crystal transformation and melting) occurred. Combined with a verification test at 180 °C for two days, it is concluded that boron and KNO3 components are stable at 180 °C. With the increase of boron content, the thermal stability of BPN sample improved, and the best performance was achieved when the ratio was 25:75 (B:KNO3).
BPN samples without binder have the best thermal stability. In the 5 day 180 °C test, the binder affected the weight loss and p-t curve of BPN. Finally, BPN with fluororubber binder is better than BPN with unsaturated polyester binder.

Author Contributions

Conceptualization, C.L. and N.Y.; methodology, C.L. and Z.L.; formal analysis, N.Y.; data curation, J.H. and N.Z.; writing—original draft preparation, C.L.; writing—review and editing, N.Y. and Y.Y.; visualization, X.H.

Funding

This research was funded by Beijing Space Vehicle General Design Department.

Acknowledgments

Thanks for the support from State Key Laboratory of Explosive Science and Technology, Yunliang Lao’s guidance in the field of thermal analysis, and the funding and experimental support from Beijing Space Vehicle General Design Department.

Conflicts of Interest

The authors declare no conflict of interest.

References

  1. Shi, C.H. In–line ignition system and its acceptable charge. Initiat. Pyrotech 1997, 01, 48–52. [Google Scholar]
  2. MIL–STD–1901A. Munition Rocket and Missile Motor Ignition System Design, Safety Criteria. 2002. [Google Scholar]
  3. Zou, Y.L.; Ouyang, Z.Y.; Xu, L.; Liu, J.J.; Xu, T. Lunar surface environment characteristics. Quat. Sci. 2002, 22, 533–539. [Google Scholar]
  4. Carl, S.; Gorzynski, J.R.; Maycock, J.N. Explosives and pyrotechnic propellants for use in long–term deep space mis–sions. J. Spacecr. Rocket. 1974, 11, 211–212. [Google Scholar]
  5. Macdonald, M.; Badescu, V. The International Handbook of Space Technology; Springer: Berlin, Germany, 2014; pp. 230–232. [Google Scholar]
  6. Rani Krishan, K.R.; Anandavally Ammal, R.; Hariharanath, B.; Rajendran, A.G.; Kartha, C.B. Addition of RDX/HMX on the Ignition Behaviour of Boron–Potassium Nitrate Pyrotechnic Charge. Def. Sci. J. 2006, 56, 329–338. [Google Scholar]
  7. Turcotte, R.; Fouchard, R.C.; Turcotte, A.M.; Jones, D.E.G. Thermal analysis of black powder. J. Therm. Anal. Calorim. 2003, 73, 105–118. [Google Scholar] [CrossRef]
  8. Pouretedal, H.R.; Ebadpour, R. Application of non–isothermal thermogravimetric method to interpret the decomposition kinetics of NaNO3, KNO3, and KClO4. Int. J. Thermophys. 2014, 35, 942–951. [Google Scholar] [CrossRef]
  9. Freeman, E.S. The kinetics of the thermal decomposition of potassium nitrate and of the reaction between potassium nitrite and oxygen. J. Am. Chem. Soc. 1957, 79, 838–842. [Google Scholar] [CrossRef]
  10. Hosseini, S.G.; Eslami, A. Thermoanalytical investigation of relative reactivity of some nitrate oxidants in tin–fueled pyrotechnic systems. J. Therm. Anal. Calorim. 2010, 101, 1111–1119. [Google Scholar] [CrossRef]
  11. Eslami, A.; Hosseini, S.G.; Pourmortazavi, S.M. Thermoanalytical investigation on some boron–fuelled binary pyrotechnic systems. Fuel 2008, 87, 3339–3343. [Google Scholar] [CrossRef]
  12. Zeng, X. Experimental and Theoretical Studies on the Thermal Stability of Nitrates. Ph.D. Dissertation, Nanjing University of Science and Technology, Nanjing, China, June 2007; p. 02. [Google Scholar]
  13. Qi, H.T.; Zhang, J.L. Processing technology and formulation design of ignition composition of boron/ultra–fine potassium nitrate. Chin. J. Ener. Mater. 2011, 19, 180–183. [Google Scholar]
  14. Wang, L.; Xu, W.Z.; Wang, J.Y. Study on preparation and peoperities of boron–potassium nitrate igniter. Chem. Intermed. 2010, 11, 38–41. [Google Scholar]
  15. Lv, Q.l. Preparation of boron/potassium nitrate (BPN) ignition charge and analysis of the effect of particle size on its properties. In Proceedings of the 11th Annual Conference of the Chinese Ordnance Institute of Pyrotechnics, Guangxi, China, 18–22 May 2001; pp. 217–220. [Google Scholar]
  16. Shen, R.Q.; Ye, Y.H.; Hu, Y.; Wang, Z.G. Laser Ignition Performance of Boron-Potassium Nitrate Composite at Different Oxygen/Fuel Ratio. Chin. J. Lasers 2009, 36, 338–341. [Google Scholar]
  17. Rugunanan, R.A.; Brown, M.E. Reactions of powdered silicon with some pyrotechnic oxidants. J. Therm. Anal. Cal–orim 1991, 37, 1193–1211. [Google Scholar] [CrossRef]
  18. GJB 5381.10–2005. Methods of Chemical Analysis for Pyrotechnic, Part 10: Determination of Potassium Nitrate Content–Sodium Tetraphenylboron Method. Chinese Military Standard. 2005. [Google Scholar]
  19. GJB 5309.23–2004. Test Methods of Initiating Explosive Devices. Part 23: Measurement of Function Alsynchronization Electron–Optical Method, Chinese Military Standard. 2004. [Google Scholar]
  20. GJB 5309.9–2004. Test Methods of Initiating Explosive Devices. Part 9: Electric–Fire Sensitivity Test, Chinese Military Standard. 2004. [Google Scholar]
Figure 1. Experimental process scheme.
Figure 1. Experimental process scheme.
Applsci 09 03630 g001
Figure 2. (a) Thermogravimetric-Differential Scanning Calorimetry (TG₋DSC) curve of boron powder; (b) TG-DSC curve of KNO3 (in nitrogen atmosphere).
Figure 2. (a) Thermogravimetric-Differential Scanning Calorimetry (TG₋DSC) curve of boron powder; (b) TG-DSC curve of KNO3 (in nitrogen atmosphere).
Applsci 09 03630 g002
Figure 3. (a) TG–DSC curve of 1#BPN (15:85); (b) TG–DSC curve of 2#BPN (25:75); (c) TG–DSC curve of 3#BPN (33:67) (heating rate 5 °C/min).
Figure 3. (a) TG–DSC curve of 1#BPN (15:85); (b) TG–DSC curve of 2#BPN (25:75); (c) TG–DSC curve of 3#BPN (33:67) (heating rate 5 °C/min).
Applsci 09 03630 g003
Figure 4. The apparent morphology of KNO3 compared before and after different temperature tests.
Figure 4. The apparent morphology of KNO3 compared before and after different temperature tests.
Applsci 09 03630 g004
Figure 5. The apparent morphology of boron compared before and after different temperature tests.
Figure 5. The apparent morphology of boron compared before and after different temperature tests.
Applsci 09 03630 g005
Figure 6. The apparent morphology of 4#BPN compared before and after different temperature tests.
Figure 6. The apparent morphology of 4#BPN compared before and after different temperature tests.
Applsci 09 03630 g006
Figure 7. DSC curves of 4#BPN 60 °C,4 h samples and 180 °C samples (heating rate 5 °C/min).
Figure 7. DSC curves of 4#BPN 60 °C,4 h samples and 180 °C samples (heating rate 5 °C/min).
Applsci 09 03630 g007
Table 1. Samples of pure components and mixtures.
Table 1. Samples of pure components and mixtures.
No.ComponentComposition (%)Binder
1Boron100--
2KNO3100--
31#BPN15:85--
42#BPN25:75--
53#BPN33:67--
64#BPN25:75Fluorine rubber
75#BPN25:75Unsaturated polyester
Table 2. Analysis methods for BPN thermal analysis and high temperature stability analysis.
Table 2. Analysis methods for BPN thermal analysis and high temperature stability analysis.
Analysis MethodContent
ThermogravimetryMeasure the weight of loose sample before and after high temperature test with precision balance.
AppearanceScanning microscope, optical digital microscope used to observe the color, particle size, etc.
DSC analysisAnalyze the initial decomposition temperature and peak decomposition temperature of samples.
Content analysisIon exchange method for determination of KNO3 contentMannitol complex titration method for determination of boron.
output performanceP–t curve pressure peak and rise time to evaluate the power capacity of samples.
Table 3. Weight statistics of potassium boron nitrate samples at different temperatures.
Table 3. Weight statistics of potassium boron nitrate samples at different temperatures.
SamplesWeight Ratio @ 100 °C (%)Weight Ratio @ 200 °C (%)Weight Ratio @ 400 °C (%)Weight Ratio @ 500 °C (%)Weight Ratio @ 650 °C (%)
1#BPN (15:85)99.398.394.888.657.5
2#BPN (25:75)99.998.593.292.775.7
3#BPN (33:67)100.099.197.494.272.5
Table 4. Peak temperature of DSC with different ratios of BPN.
Table 4. Peak temperature of DSC with different ratios of BPN.
SamplesFirst Endothermic Peak (°C)Second Endothermic Peak (°C)Exothermic Peak (°C)
1#BPN (15:85)133.6332.0547.4
2#BPN (25:75)134.8331.3534.6
3#BPN (33:67)136.5332.6526.2
Table 5. DSC parameter comparison of 4#BPN sample (°C) (heating rate 5 °C/min).
Table 5. DSC parameter comparison of 4#BPN sample (°C) (heating rate 5 °C/min).
Parametric60 °C, 4 h180 °C, 2 days180 °C, 5 days
Initial temperature of first endothermic peak (°C)129.04129.45128.84
First endothermic peak (°C)131.15131.35131.55
Initial temperature of second endothermic peak (°C)334.95335.12335.35
Second endothermic peak (°C)336.02336.06336.23
Initial temperature of exothermic peak (°C)405.34406.37404.33
Exothermic peak (°C)431.28424.77428.51
Decomposition heat E (J·g−1)344734543367
Energy loss rate 1 (%)01.013.26
1 Energy loss rate: (E60°C4h–E180°C, xd)/E60°C4h.
Table 6. Weight loss ratios of BPN samples in 180 °C test.
Table 6. Weight loss ratios of BPN samples in 180 °C test.
Sample 1Weight Loss Ratio after 60 °C, 4 h (%)Weight Loss Ratio after 180 °C, 2days (%)Weight Loss Ratio after 180 °C, 5days (%)
1#BPN (15:85)0.0970.120.11
4#BPN (25:75)0.3721.040.98
5#BPN (25:75)0.0951.191.59
KNO30.00830.044--
Boron1.5495.26--
1 Binders of 4#BPN, 5#BPN are fluorine rubber, and unsaturated polyester, respectively.
Table 7. Component variation of BPN samples in 180 °C test [18].
Table 7. Component variation of BPN samples in 180 °C test [18].
SampleComponent60 °C, 4 h (%)180 °C, 2 days (%)180 °C, 5 days (%)
1#BPN (15:85)KNO3 (%)85.8085.6685.90
Boron (%)14.8714.8814.85
4#BPN (25:75) KNO3 (%)73.3273.7974.36
Boron (%)23.0427.3826.24
Table 8. P-t curve of BPN samples in 180 °C test [19,20].
Table 8. P-t curve of BPN samples in 180 °C test [19,20].
Sample ComponentPeak Pressure (MPa)Rise Time (ms)Rate of Peak Pressure Change (%)
1#BPN (15:85)60 °C, 4 h2.113.09−0.95
180 °C, 5 days2.092.94
4#BPN (25:85)60 °C, 4 h2.571.82−10.89
180 °C, 5 days2.291.33
5#BPN (25:75)60 °C, 4 h3.344.09−25.75
180 °C, 5 days2.484.59

Share and Cite

MDPI and ACS Style

Li, C.; Yan, N.; Ye, Y.; Lv, Z.; He, X.; Huang, J.; Zhang, N. Thermal Analysis and Stability of Boron/Potassium Nitrate Pyrotechnic Composition at 180 °C. Appl. Sci. 2019, 9, 3630. https://0-doi-org.brum.beds.ac.uk/10.3390/app9173630

AMA Style

Li C, Yan N, Ye Y, Lv Z, He X, Huang J, Zhang N. Thermal Analysis and Stability of Boron/Potassium Nitrate Pyrotechnic Composition at 180 °C. Applied Sciences. 2019; 9(17):3630. https://0-doi-org.brum.beds.ac.uk/10.3390/app9173630

Chicago/Turabian Style

Li, Chaozhen, Nan Yan, Yaokun Ye, Zhixing Lv, Xiang He, Jinhong Huang, and Nan Zhang. 2019. "Thermal Analysis and Stability of Boron/Potassium Nitrate Pyrotechnic Composition at 180 °C" Applied Sciences 9, no. 17: 3630. https://0-doi-org.brum.beds.ac.uk/10.3390/app9173630

Note that from the first issue of 2016, this journal uses article numbers instead of page numbers. See further details here.

Article Metrics

Back to TopTop