A numerical and experimental study of the decomposition ... · A numerical and experimental study...
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A numerical and experimental study of the decompositionpathways of guanidinium nitrate
Anand Sankaranarayanan1 • Lovely Mallick2 • Neeraj R. Kumbhakarna1
Received: 1 November 2016 / Accepted: 12 September 2017
� Akademiai Kiado, Budapest, Hungary 2017
Abstract The thermal decomposition behaviour of guani-
dinium nitrate (GN), an energetic material, was analysed
using a combined experimental and computational
approach. Simultaneous thermogravimetric analysis,
Fourier transform infrared spectroscopy and mass spec-
trometry (TG-FTIR-MS) experiments were carried out at
three different heating rates under closed and open crucible
conditions. A two-stage decomposition process was
observed, and the major gases evolved were found to be
NH3, N2O, NO2 and CO2. Quantum mechanics based
ab initio computations were performed to evaluate the
possible decomposition pathways available for GN. Results
indicate that decomposition of GN is not initiated in the
condensed phase as the guanidinium cation and the nitrate
anion are highly stable. The most likely mechanism
involves isomerization of GN followed by a proton transfer
in the gas phase to yield nitric acid and guanidine. These
products then further react to form nitroguanidine (NQ)
and H2O. NQ dissociates via several competing pathways
to yield NH3, N2O, H2O and CO2. HNO3 decomposition
can help explain NO2 formation. The residue left towards
the end of TG can be attributed to dimerization and
trimerization reactions of cyanamide.
Keywords Guanidinium nitrate � Thermal decomposition �Energetic material � TG–FTIR–MS � Ab initio
computations
Introduction
Guanidinium nitrate (GN) is a very stable compound [1]
commonly used as a gas-generating agent [2, 3] and in
solid propellant formulations [4]. GN is used to produce
nitroguanidine (NQ) [5], also known as picrate, which is a
secondary explosive often used in triple-base formulations
as a gun propellant and in impact insensitive military
ammunition [6]. The molecular structure of GN is shown in
Fig. 1.
The decomposition study of any propellant can help us
formulate detailed chemical reaction mechanisms with
which the combustion behaviour of the same can be
modelled [7]. Such modelling can be helpful in controlling
emissions and also provide us valuable guidelines regard-
ing the best practices to be followed during handling,
storage, transportation and disposal of these compounds
[8]. These studies also provide information which could aid
the development of better propellants in the future. Meth-
ods like differential thermal analysis (DTA), thermo-
gravimetric (TG) analysis and differential scanning
calorimetry (DSC) are the most commonly used diagnostic
tools, deployed to gain insights on the decomposition
behaviour of any energetic material [9–12].
One of the earliest studies on the decomposition beha-
viour of guanidine salts, to assess their thermal stability,
was carried out by Fauth [13]. Investigations were done
using DTA and TG, under conditions involving heating
rates of 8 �C per minute. Decomposition of GN was found
to be initiated at temperatures of around 100 �C and was
Electronic supplementary material The online version of thisarticle (doi:10.1007/s10973-017-6707-4) contains supplementarymaterial, which is available to authorized users.
& Neeraj R. Kumbhakarna
1 Department of Mechanical Engineering, Indian Institute of
Technology, Bombay, Mumbai 400076, India
2 Department of Aerospace Engineering, Indian Institute of
Technology, Bombay, Mumbai 400076, India
123
J Therm Anal Calorim
DOI 10.1007/s10973-017-6707-4
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95% complete at 250 �C. Mass spectral study of GN, along
with simultaneous TG–DTA studies, was carried out by
Udupa [14]. The TG–DTA studies were performed in an
argon atmosphere, with a heating rate of 4 �C per minute.
The DTA curve was reported to have an endotherm at
210 �C and an exotherm at 305 �C. The endothermic and
exothermic peaks were attributed to the melting of GN and
to the oxidative decomposition of GN, respectively. The
decomposition of GN was found to commence at 230 �Cand achieved completion by 500 �C. It was observed to be
fast between 275 and 325 �C and sluggish in the temper-
ature range 325–500 �C. The mass spectral results at
230 �C suggested the initiation of decomposition through a
proton transfer mechanism. Wendlandt et al. [4] reported
TG and DSC curves for guanidinium salts in the temper-
ature range between 25 and 500 �C. The studies were done
in a dynamic N2 environment with heating rates of 10 �Cper minute. The authors report a gradual mass loss for GN
beginning at around 50 �C with the main apparent disso-
ciation occurring at around 215 �C. The exothermic peak at
305 �C reported by Udupa [14] was not observed in this
study. The anomaly was thought to be caused due to dif-
ference in the sample size, design of sample container and
heating rates. Oxley et al. [15] reported the activation
energy (Ea) and pre-exponential factor (A) values for the
decomposition of GN under isothermal heating conditions
and proposed three possible decomposition routes of GN:
first involving deprotonation, second proceeding by dehy-
dration and the third resulting in ammonium nitrate as an
intermediate. Decomposition route via formation of urea
was ruled out as neither urea nor its decomposition prod-
ucts were observed. Damse [16] investigated the cause for
fast burning behaviour of triaminoguanidine azide
(TAGAZ). As a part of this study, TG, DTA and DSC
studies were performed to understand the thermal beha-
viour of TAGAZ and GN. In addition, hyphenated tech-
niques of thermogravimetry–Fourier transformer infrared
spectroscopy (TG–FTIR) and pyrolyser–gas chromatogra-
phy–mass spectroscopy (Py–GC–MS) were also used in
order to find out the decomposition gases. It was concluded
that the decomposition of GN proceeded through the dis-
sociation of relatively strong C–N bonds. FTIR results
indicated evolution of NH3 and HCN during the first and
second stages of decomposition, respectively. An exotherm
was reported between 290 and 325 �C with a peak at
303.17 �C. Mei et al. [3] investigated the thermal decom-
position of GN and basic cupric nitrate mixtures using
thermogravimetry–differential scanning calorimetry–mass
spectrometry–Fourier transform infrared spectroscopy
(TG–DSC–MS–FTIR) and automatic calorimeter. Results
of pure GN samples were also reported. The onset of GN
decomposition was reported to occur at 278 �C. 72.8% of
the sample was found to be dissociated by 320 �C. The
authors report no exothermic peaks for decomposition of
pure GN.
Studies on thermal decomposition behaviour of
nitroguanidine (NQ), a dehydration product of GN, can be
found in literature [17]. NQ was found to be relatively
stable below its melting point of approximately 230 �C,
above which it decomposed, evolving ammonia and water
vapour, and forming solid products. The major intermedi-
ates identified during the decomposition of NQ were
nitrous oxide, cyanamide, melamine, cyanic acid, cyanuric
acid, ammeline and ammelide. The compounds, on further
decomposition, yielded carbon dioxide, urea, nitrogen,
hydrogen cyanide, cyanogen and other compounds not yet
fully confirmed, such as melam, melem and mellon prob-
ably containing condensed triazine rings. Most of the
products reported during NQ decomposition have been
observed for GN decomposition as well, indicating that NQ
could be an intermediate during GN decomposition. There
is no available literature on the use of ab initio computa-
tional methods to assess the decomposition behaviour of
GN to the best of the authors’ knowledge. How-
ever, studies on guanidine derivatives [18–20] may provide
useful insights in this regard. These studies reveal that
guanidinium azotetrazolate (GzT) and guanidinium
5-amino tetrazolate (GA) do not allow for a proton transfer
in the condensed phase. Their condensed phase decompo-
sition proceeds though the dissociation of the anion frag-
ments. Similar results can be expected for GN. The
dissociation of the nitrate anion is, however, unlikely as it
is quite stable.
Although much work has been done in the past few dec-
ades on studying the thermal decomposition behaviour of
GN, they have been inconclusive on the exact decomposition
mechanism of GN. Inconsistency in experimental data
reported in separate studies has also been noted. Some of
these studies have been performed with equipment which are
nowadays considered obsolete. It is therefore imperative to
revisit the decomposition study of GN. Developing a
detailed chemical kinetic mechanism (DCKM) for GN
decomposition could also prove to be beneficial for future
studies in this area. The present work attempts to elucidate
the reaction mechanism for GN decomposition while vali-
dating experimental results from previous studies.
NC
+
N
N
H
H
H
H
HH
N+
O-
O-
O
Fig. 1 Molecular structure of guanidinium nitrate
A. Sankaranarayanan et al.
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The technique chosen for this purpose was the
hyphenated TG–FTIR–MS method, supported by quantum
mechanics based ab initio calculations. GN was subjected
to testing under three distinct heating rates to extract the
variation of global activation energies and pre-exponential
factors with the reacted mass fraction using iso-conver-
sional methods and the kinetic compensation effect. The
TG and TDG curves were plotted to identify decomposi-
tion patterns and the temperature regimes of their occur-
rence. The gas species evolved during the process were
identified using FTIR spectroscopy. The mass spectra,
though uncalibrated, served as a valuable corroboration of
the data obtained from the FTIR spectra. Ab initio com-
putations were then performed to explain the formation of
product gases detected during experiments.
Methodology for experimental and numericalwork
The decomposition of GN was studied using the hyphen-
ated TG–FTIR–MS method. FTIR and MS, when used
alongside TG, have been found to be synergistic in nature,
as the complete spectrum of the evolved gases is revealed
by either of the instruments. A detailed description of the
experimental set-up used for our present study is given in
Reference [21]. A brief description of the same along with
the experimental procedure employed for our present work
is given here. The particle size distribution of GN used for
our experiments along with digital microscopic images of
the same has been provided in Online Resource 1. Tests
were conducted under open and pierced lid conditions with
approximately 2 mg of the GN sample placed in an alu-
mina crucible. A constricting lid with 0.1-mm hole at the
centre was used to cover the crucible for the pierced lid
tests. The thermal decomposition process of GN was
studied by using Netzsch 209 thermogravimetry analyser,
with heating rates of 5, 10 and 15 K min-1.
The computational part of the present work was carried
out with the help of Gaussian 09 [22] suite of programs.
Preliminary investigations for ground-state and transition-
state optimizations were done using the B3LYP density
function theory with 6-31?? G(d,p) basis set [23, 24]. The
more accurate CBS-QB3 [25] compound method was used to
recalculate the values which have been reported for the
reaction pathways listed in this paper. The same has been
recognized to provide a good balance between accuracy of
results and computational resources required for calculations
[26, 27]. Further details of the methodology adopted for
numerical simulations can be found in Online Resource 2.
Results and discussion
TG Data and Kinetic Analysis
The TG and DTG plots of GN crystals subjected to a
heating rate of 15 K min-1 are presented in Fig. 2. The
samples were analysed under two crucible conditions: open
condition (oc) and pierced lid condition (cc). All experi-
ments were repeated thrice with similar test conditions, and
the average values were used for plotting the results.
The first stage of the decomposition process, between
260 and 336 �C, was observed to be fast with 75% mass
loss. The second stage was found to be sluggish in com-
parison to the first stage with a mass loss of approximately
10% and left 15% residues at the end temperature of
500 �C. The DTG peak was observed towards the end of
the first stage at a temperature of around 314 �C for GNoc
and GNcc. Similar trends have been reported by other
researchers [14, 16]. The onset and extent of decomposi-
tion, however, varied according to the experimental con-
ditions. The TG curves and the DTG peaks for closed and
open crucible tests were found to nearly overlap each other
with the rate of mass loss percentage of TGcc being higher
than that of TGoc. The occurrence of a two-stage decom-
position process can be understood by plotting the variation
of the global activation energy (Ea) with the reacted mass
fraction, a. The same has been shown in Fig. 3 for GNoc
and GNcc. Ea was calculated using the procedure outlined
in our previous work [21], with heating rates of 5, 10 and
15 K min-1. The curves were found to follow similar
trends, with the first four points constituting the fast
decomposition stage and fourth and fifth points
Temperature/°C
Mas
s/%
DTG
/% m
in–1
100 200 300 400 5000
20
40
60
80
100
–6
–5
–4
–3
–2
–1
0
TGOCDTGOCTGCCDTGCC
Fig. 2 TG–DTG of GNoc and GNcc at a heating rate of 15 K min-1
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representing the slow decomposition stage as apparent
from the sudden increase in Ea value.
The activation energies of GNoc and GNcc were found to
be approximately constant from a = 0.1 to 0.8 with aver-
age values of 139 and 156 kJ/mol, respectively. The pre-
exponential factors (A) for open and pierced lid conditions
were found to be 2.64 9 109 and 7.53 9 1010 min-1,
respectively. The Ea increased considerably, henceforth, till
it attained a maximum of 201 and 239 kJ/mol at a = 0.9
for GNoc and GNcc, respectively. The activation energy
(Ea) and pre-exponential factor (A) of recrystallized GN,
under isothermal heating conditions, reported in [15] were
199 kJ/mole and 1.94 9 1015 s-1, respectively. Purity of
the GN sample, particle size distribution, heating rates,
sample size, crucible conditions and nature and flow rate of
purge gas are some of the factors which can affect the
results.
TG–FTIR analysis
The FTIR spectra of the evolved gases during the decom-
position process of GNoc and GNcc for a heating rate of
15 K min-1, at various junctures, are shown in Figs. 4 and
5, respectively. The quantity of the evolved gases was too
minute to be detected at the decomposition onset temper-
ature of 285 �C. The second spectrum was taken at a
temperature of 314 �C, corresponding to the maximum of
the DTG signal. The major species detected were CO2,
HNCO, N2O, HNO3, NO2 and NH3. In this stage, the
intensities of N2O and NH3 were high, while that of HNO3
was low. The intensities of CO2, HNCO and N2O were
found to be interdependent and varying. The end of the fast
decomposition phase was marked by the high transmittance
values of the third spectrum, taken at a temperature of
333 �C. The fourth spectrum, at 409 �C, corresponds to the
Reacted fraction
E a/k
Jmol
–1
0 0.2 0.4 0.6 0.8 1
140
160
180
200
220
240GNOCGNCC
Fig. 3 Comparison of activation energies with reacted fraction
during decomposition of GNoc and GNcc
100015002000250030003500
0.97
0.98
0.99
1
1
1
1
1
(a)
0.97
0.98
0.99
(b)HNO3
N2ONO2N2O NH3
CO2
Tran
smitt
ance
0.97
0.98
0.99
(c)
0.97
0.98
0.99
(d)NH3
NO2
N2ON2O
CO2 HNCO
Wavenumber/cm–1
1000150020002500300035000.97
0.98
0.99
(e)
Fig. 4 FTIR spectra of evolved gases during decomposition of GNoc at 15 K min–1; (a) T = 285 �C, (b) T = 314 �C, (c) T = 333 �C, (d)T = 409 �C and (e) T = 500 �C
A. Sankaranarayanan et al.
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middle of the second stage of decomposition, and the last
spectrum shown in Figs. 4(e) and 5(e) represents the end of
the programmed temperature, at 500 �C.
In order to further understand the kinetics of the reac-
tions governing the decomposition of GN, the FTIR spectra
of the evolved gases were quantified using the iterative
procedure described in our previous work [21]. The results
for open and pierced lid conditions obtained using the same
are respectively displayed in Figs. 6 and 7.
The figures show the variation of relative mole fractions
of various species with temperature, which appear in the
ppm range, owing to the overabundance of nitrogen as the
purge gas. It is clear from both the figures that NH3 and
N2O are the dominant species. H2O was detected only for
open condition. The ratio of the mole fractions of various
species with respect to that of NO2, at the temperature
where the FTIR signals were the strongest, is shown in
Table 1. The mole fraction of CO2 was comparable to that
100015002000250030003500
0.97
0.98
0.99
1
1
1
1
1
(a)
0.97
0.98
0.99
(b) N2ONO2N2O NH3
CO2
Tran
smitt
ance
0.97
0.98
0.99
(c)HNCO
0.97
0.98
0.99
(d)NH3
NO2
N2ON2O
CO2
Wavenumber/cm–1
1000150020002500300035000.97
0.98
0.99
(e)
Fig. 5 FTIR spectra of evolved gases during decomposition of GNcc at 15 K min–1; (a) T = 285 �C, (b) T = 314 �C, (c) T = 333 �C, (d)T = 409 �C and (e) T = 500 �C
Temperature/°C
Rel
ativ
e m
ole
frac
tion/
%
Mas
s los
s/%
250 300 350 400 450 500
0.02
0.04
0.06
0.08
0.1
0.12
20
40
60
80
100NH3N2OH2ONO2CO2HNO3TGOC
Fig. 6 Relative mole fraction of evolved gases quantified from FTIR
spectra during decomposition of GNoc at 15 K min-1
Temperature/°C
Rel
ativ
e m
ole
frac
tion/
%
Mas
s los
s/%
250 300 350 400 450 5000
0.02
0.04
0.06
0.08
0.1
0.12
20
40
60
80
100NH3N2OH2ONO2CO2HNO3TGCC
Fig. 7 Relative mole fraction of evolved gases quantified from FTIR
spectra during decomposition of GNcc at 15 K min-1
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of NO2, while that of HNO3 found to be considerably lower
than NO2.
TG–MS analysis
The mass spectra revealed a wider array of species as
compared to the FTIR spectra. Major peaks were obtained
corresponding to m/z = 16, 17, 18 and 44. These values
can be assigned to O/NH2, NH3/OH, H2O and CO2/N2O,
respectively. In addition to this, smaller signals were also
detected at m/z = 12, 14, 20, 22, 23, 26, 28, 32, 34, 36, 40,
41, 42, 43, 45 and 46. Important among these corresponds
to CO/N2 (m/z = 28), H2NCN/NHCNH (m/z = 42),
HNCO (m/z = 43) and NO2 (m/z = 46). The result is
somewhat consistent with those obtained in previous
studies [14, 16]. The signals corresponding to the species
NH3, N2O, NO2, CO2, H2O and HNCO, identified in FTIR,
were confirmed through MS.
SEM analysis of GN
In our previous work [21], the nature of ammonium per-
chlorate (AP) particles was studied under various condi-
tions. The porosity observed in the microstructure under
specific conditions helped to understand the complexity of
AP decomposition to a certain extent. Similar studies on
Table 1 Ratio of relative mole fractions (%) of various species obtained during decomposition of GN at 15 K min-1
Temperature (314 �C) N2O: NO2 NH3: NO2 CO2: NO2 HNO3: NO2
GNoc 4.68 8.01 1.40 0.44
GNcc 2.88 4.59 1.10 0.17
Fig. 8 SEM images of the decomposition of GNoc (a, b, c) at 313 �C and GNcc (d, e, f) at 317 �C for a heating rate of 15 K min-1
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GN particles at various temperatures and crucible condi-
tions are crucial in understanding its decomposition
mechanism. The GN samples were subject to TG tests
under open and pierced lid conditions, at a heating rate of
15 K min-1, as explained in the ‘‘TG Data and Kinetic
Analysis’’ section. The end of programmed temperature for
GNoc and GNcc was chosen as 313 and 317 �C, respec-
tively, based on the DTG peaks of the compound. The
samples were removed from the crucible on completion of
the tests, with the help of a spatula and stored in a dry
place. Morphologies of the samples thus obtained were
analysed using a JSM–7000F field emission gun scanning
electron microscope. Figure 8 shows SEM images of GN
samples, visualized using varying scales, for open and
pierced crucible tests. The particles from open crucible
tests were found to be larger in size than those from pierced
lid tests, where they were observed to be fragile and had
fragmented into smaller pieces. Anomalies in
Table 2 Condensed phase decomposition pathways for guanidinium nitrate with thermodynamic parameters computed at CBS-QB3 level of
theory
No Reaction DHRa D�Hf
b D�Hbc DGR
d D�Gfe D�Gb
f
R1GN INT 1_c
TS1_c 90.4 211.3 120.9 109.5 264.7 138.7
R2TS2_c
INT1_c + N
O
OOH
NH2NH2
NH
2.6 5.7 3.1 -3.0 3.4 6.9
R3 NH2NH2
NH
+ N
O
OOH
TS3_c
NH
NH2 NHN
O
O
+ OH2
7.4 106.5 99.1 0.3 239.9 239.6
R4 TS4_cONO2
–NO3
–230.6 432.5 201.9 222.6 490.9 234.8
R5TS5_c
ONO2–G+ + +
NH2NH2
NH
N
OO
O
H
1.3 -3.2 -4.4 2.5 8.0 5.0
R6TS6_c
N
O
OOH
N
OO
O
H
-144.3 137.2 281.5 -132.4 156.8 309.1
R7 TS7_cG+ INT2_c
111.9 211.2 99.3 124.9 265.8 122.1
R8 TS8_cINT2_c INT3_c
11.0 82.4 71.5 10.3 78.1 66.3
R9 TS9_cINT3_c NH4
+ + C NNH
H 7.3 86.1 78.8 -85.8 77.0 175.8
R4 has been computed at B3LYP level of theory using 6-31??G(d,p) basis set
_c has been used to denote condensed phase reactionsa Enthalpy of reaction (kJ/mol)b Activation enthalpy in the forward direction (kJ/mol)c Activation enthalpy in the backward direction (kJ/mol)d Gibbs free energy of reaction (kJ/mol)e Gibbs free energy of activation in the forward direction (kJ/mol)f Gibbs free energy of activation in the backward direction (kJ/mol)
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microstructure or nuclei formation on the surface were not
found, which may be indicative of decomposition process
dominating over sublimation.
Numerical simulations
Condensed phase reactions
As the objective of the numerical simulation was to explain
the species detected in the experimental studies, the con-
densed phase mechanisms were explored first. The path-
ways involving proton transfer, dehydration of GN and
formation of ammonium nitrate as an intermediate during
GN decomposition, as suggested by Oxley et al. [15], were
explored. A mechanism involving a single-step proton
transfer to form HNO3 could not be found in the condensed
phase. The result was similar to those obtained for guani-
dine derivatives GA and GzT [19, 20], where the decom-
position was initiated through the rupture of the anionic
fragments. Two mechanisms, one involving isomerization
of GN and another involving isomerization of NO3- to form
ONO2-, were hence explored but found to have high acti-
vation energies and low rate constants. The possibility of
guanidinium ion (G?) decomposing to form NH4? ion was
also investigated and found to be improbable. Condensed
phase reactions obtained, pertaining to initiation of GN
decomposition, are presented in Table 2 along with rele-
vant thermodynamic parameters. The CBS-QB3-optimized
structures of some of the compounds of interest in the
condensed phase are shown in Fig. 9.
Gas-phase initiation reactions
Since the condensed phase reactions did not yield any
promising decomposition pathways, the gas-phase decom-
position mechanism of GN was also explored. Transition
states were obtained for different reactions corresponding
to the stable isomer of GN. The major reaction pathways
identified were (1) isomerization of GN to yield the inter-
mediate INT1, (2) decomposition of GN to guanidine and
HNO3 and (3) decomposition of GN to nitroguanidine and
H2O. Although a reaction involving a single-step proton
was found to occur for GN, the more likely pathway on
account of lower activation energies and higher rate con-
stant is via the formation of INT1. Reaction corresponding
to dehydration of INT1 to yield nitroguanidine was also
found. The structures corresponding to the lowest energy
state for GN and INT1, after ground-state optimization at
CBS-QB3 level of theory in gas phase, are presented in
Fig. 10, and a summary of the explored initiation reactions
involving gas-phase decomposition of GN is presented in
Table 3.
Decomposition of GN was found to be initiated by the
reaction involving isomerization of GN to INT1, as the
same had the lowest activation energy and the highest rate
constants among the explored pathways. INT1 would then
decompose to form guanidine and HNO3. These products
then react to form NQ and H2O, once sufficient concen-
tration of Gu and HNO3 is built-up. The reaction involving
GN
INT2_c
INT1_c
INT3_c
Fig. 9 Optimized structure of GN and intermediates in condensed
phase
GN INT1
Fig. 10 Optimized structures for guanidinium nitrate and intermedi-
ate 1 in gas phase
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Table 3 Decomposition pathways for guanidinium nitrate in gas phase with thermodynamic parameters computed at CBS-QB3 level of theory
No Reaction DHRa D�Hf
b D�Hbc DGR
d D�Gfe D�Gb
f
(R10)GN
TS1INT 1
21.0 15.5 -5.6 19.6 26.6 7.0
(R11)
GN TS2 NH2
NH
NH2
+OH
N
O
O
86.3 189.7 103.4 10.0 208.0 198.0
(R12)
GN TS3
NH
NH H
NN
O
O
H
NQ
+ OH2
36.5 228.8 192.3 -32.4 249.9 282.3
(R13)
GN TS4
NH2
NH2
NQ0
NN
O
O
+ OH2
2.0 258.6 256.6 -67.9 274.5 342.3
(R14)
INT 1TS5
NH2
N
NH2
H
+H
N
O
OO
1.7 -2.6 -4.3 -1.1 5.2 6.2
(R15)
INT 1 + OH2
TS6N
H
NH H
NN
O
O
H
NQ
15.4 196.8 181.4 -52.0 218.4 270.4
(R16) NH2NH2
NH
+ N
O
OOH
N
O
OOH+ NH3 + N C NH2
TS766.6 226.7 160.1 -32.7 308.5 341.2
(R17) NH2NH2
NH
NH3N C NH
HTS8
+
77.3 213.9 136.6 -20.6 216.2 236.7
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formation of NQ was found to be exothermic which is
typical of nitration reactions.
Reactions involving nitroguanidine
Two configurations of nitroguanidine have been reported in
the literature [5]. These have the formula (H2N)2–CN–NO2
and (H2N)–C(NH)NH–NO2. Several reactions involving
nitroguanidine and its isomers were explored. The
nomenclature adopted for these compounds in this paper,
along with their optimized structures, is presented in
Fig. 11. The energy values calculated at CBS-QB3 level of
theory, at a temperature of 587 K, are also reported.
NQ0 and NQ have relatively stable structures and do not
dissociate directly. In fact, the most likely pathway found
for the dissociation of NQ0 was via the formation of NQ.
NQ undergoes further reactions involving formation of
NQ1, NQ2 and NQ3. NQ1 and NQ2 follow pathways
which ultimately result in the formation of cyanamide, H2O
and N2O. The pathway involving NQ3 decomposition
yields NH3, N2O and HNCO. The reaction pathways
explored are presented in Table 4. Structures of reaction
intermediates INT2, INT3 and INT4 are provided in
Fig. 12. Several exothermic reaction steps can be traced,
which can justify the exothermic peaks reported in previ-
ous studies [14–16].
Table 3 continued
No Reaction DHRa D�Hf
b D�Hbc DGR
d D�Gfe D�Gb
f
(R18)
NH2NH2
NH
+ N
O
OOH
+
TS9
NH
NH H
NN
O
O
H
OH2
NQ
-49.8 131.6 181.4 -42.4 227.9 270.3
(R19)
NH2NH2
NH
+ N
O
OOH
TS10
N
N NN
O
O
H
H
H
H
+ OH2
NQ1
-42.1 182.1 224.1 -35.5 271.6 307.1
a Enthalpy of reaction (kJ mol-1)b Activation enthalpy in the forward direction (kJ mol-1)c Activation enthalpy in the backward direction (kJ mol-1)d Gibbs free energy of reaction (kJ mol-1)e Gibbs free energy of activation in the forward direction (kJ mol-1)f Gibbs free energy of activation in the backward direction (kJ mol-1)
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Reactions involving formation of NO2, CO2 and solid
residues
The mechanism for decomposition of HNO3 to NO2, N2O
and H2O above temperatures of 290 �C has been reported
by Oxley et al. [28]. The extent of dissociation depends on
the pressure and thus can help partially explain the varia-
tion in HNO3, NO2, N2O and H2O concentrations seen in
open and closed crucible tests. In closed crucible tests,
where some of the HNO3 remained undissociated, no traces
of H2O could be detected.
The parent molecule, GN, has only one carbon atom
which can be traced to cyanamide and HNCO as the reaction
proceeds. HNCO is known to hydrolyse to CO2 and NH3
[29]. A single-step oxidation reaction from cyanamide to
CO2 is not possible as it is strongly bound to N atoms on both
sides. Cynamide, once formed, undergoes dimerization and
trimerization reactions to form melamine and other products
which form the solid residues that remain towards the end of
the TG process. These species have been confirmed in M/S
results in previous studies [14]. The intermediate steps
involve formation of NH3 [19, 20].
Summary of GN decomposition
Based on the reactions explored, a schematic of the
important reaction pathways in the decomposition of GN is
shown in Fig. 13.
The activation energy values reported in Fig. 13 have
been computed using transition-state theory [30]. Equa-
tions for calculating reaction rate parameters from infor-
mation provided in Tables 2–4 have been provided in
Online Resource 3. The transition-state structures of all
reactions explored in this work have been provided in
Online Resource 4.
NQ0
NQ1
NQ3
NQ2
NQIsomer E (hartree)NQ0 –409.303096NQ –409.289978NQ1 –409.287017NQ2 –409.287116NQ3 –409.250647
Fig. 11 Optimized structure and electronic energy values of nitroguanidine and its isomers, computed at CBS-QB3 level of theory
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Table 4 Decomposition pathways of nitroguanidine and its isomers
No Reaction DHRa D�Hf
b D�Hbc DGR
d D�Gfe D�Gb
f
(R20)
NQ0TS1
NQ11 34.4 163.6 129.1 35.5 168.2 132.7
(R21)
NQ0TS1
NQ32 137.7 199.2 61.5 135.2 206.8 71.6
(R22)
NQ0TS13
N C NH2 + N
H
HN
O
O
93.8 343.6 249.9 -6.4 339.7 346.1
(R23)
NQTS1
NQ24 7.5 79.5 72.0 4.4 78.7 74.3
(R24)
NQTS15
N
H
C N
H
+ N
H
HN
O
O
70.1 239.5 169.4 -29.8 236.9 266.7
(R25)
NQ2TS16
N
H
C N
H
+ INT2
102.7 141.4 38.6 5.8 135.9 130.2
(R26)
H
N C N
H
+ INT2TS17
N C NH2 + N
H
HN
O
O
-50.9 33.8 84.7 -52.1 133.6 185.7
(R27)N C + INT2NH2
TS18NQ1
-91.7 50.3 142.0 8.9 146.3 137.4
(R28)
NQ1TS1
NQ29 -0.3 179.4 179.6 -2.5 177.6 180.1
(R29)
NQ1 NQ3TS20 95.5 156.9 61.4 92.8 163.1 70.3
(R30)
NQ3 INT3TS21 -46.4 43.3 89.7 -38.4 52.9 91.4
(R31)
NQ3TS22
+ NH3N C N
N
O
O
H
13.0 56.8 43.8 -88.6 35.5 124.1
(R32) TS23INT2N
H
HN
O
O
40.2 159.4 119.2 39.9 159.5 119.5
(R33) TS24H2O + N2OINT2
-200.0 131.1 331.1 -284.4 124.9 409.3
(R34)TS25
N C N
H
H
N C NH2
-10.8 322.9 333.6 -12.1 321.1 333.2
(R35)
INT3TS26
+ NH3N C N
N
O
O
H
59.4 86.8 27.4 -50.2 71.0 121.2
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Conclusions
GN is a very stable compound and does not decompose easily.
In this work, the experimental studies revealed that at 1
atmospheric pressure, the decomposition of GN commences
around 260 �C. Two distinct regimes were identified—fast
decomposition occurs at temperature ranges between 260 and
336 �C with 75% mass loss and slow decomposition occurs
from 336 to 500 �C with another 10% mass loss. These values
were in close agreement with those obtained by Udupa [14]
and Damse [16]. The major species identified from TG–
FTIR–MS were NH3, N2O, NO2, H2O and CO2.
The mechanisms for GN decomposition as proposed in
previous studies [14–16] were explored in addition to
several other pathways. The results from ab initio com-
putations indicate that decomposition of GN is unlikely in
the condensed phase on account of high activation ener-
gies and low rate constants for the initiation reactions.
The G? cation and NO3- anion being highly stable do not
decompose easily. The expected single-step proton
transfer reaction to form Gu and HNO3 was not found to
occur either in the condensed or in the gas phase. The
reactions involving direct cleavage of CN bond were also
revealed to be highly improbable. Single-step dehydration
Table 4 continued
No Reaction DHRa D�Hf
b D�Hbc DGR
d D�Gfe D�Gb
f
(R36)
TS27N C N
N
O
O
H
INT4
19.2 60.1 41.0 33.6 74.6 41.0
(R37) TS28INT4 N2O + N C O
H
-296.8 43.8 340.6 -392.5 39.6 432.1
INT2 INT3 INT4
Fig. 12 Structures of important reaction intermediates given in Table 4
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of GN to yield NQ and H2O or the formation of ammo-
nium nitrate intermediate can also be effectively ruled
out. The most probable decomposition mechanism
involves isomerization of GN to INT1 in the gas phase,
followed by a proton transfer from INT1 to yield HNO3
and guanidine. Gu and HNO3 further react, but rather
slowly to form NQ and H2O in an exothermic step. NQ
dissociates via several competing pathways to yield NH3,
N2O, H2O and CO2. HNO3 decomposition can help
explain NO2 formation. The residue left towards the end
of TG can be attributed to dimerization and trimerization
reactions of cyanamide. Thus, most of the products
observed during experiments can be explained by the
proposed reaction pathways.
Ea = 20.37 kJ/mol
GN
INT1
Ea = 2.24 kJ/mol
Ea = 141.37 kJ/mol
NO2
DECOMPOSITIONHNO3 Gu+
NQ H2O
NQ2
Ea = 84.36 kJ/mol
INT2 HNCNH
Ea = 146.24 kJ/mol
Ea = 61.64 kJ/mol
H2O
N2O
+
NH2NO2 INT2 NCNH2+
NQ1NQ3Ea = 161.81 kJ/mol
Ea = 136.03 kJ/mol
NH3
NO2NCNH
INT4Ea = 48.68 kJ/mol
HNCO
NH3
HYDROLYSIS
N2O
CO2
NH3
DIMERIZATION, TRIMERIZATION
MELAMINE
Ea = 60.07 kJ/mol
Ea = 43.53 kJ/mol
Ea = 164.26 kJ/mol
Ea = 65.02 kJ/mol
Fig. 13 Important reaction pathways in the decomposition of GN
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Acknowledgements The authors would like to acknowledge the
grants from Industrial Research & Consultancy Centre (IRCC), IIT
Bombay for supporting their project (Grant No. 14IRCCSG021). The
technical support provided by the Sophisticated Analytical Instrument
Facility (SAIF) IIT Bombay, towards conducting the SEM experi-
ments is also acknowledged.
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