Jatinder
Singh
a,
Richard J.
Staples
b and
Jean'ne M.
Shreeve
*a
aDepartment of Chemistry, University of Idaho, Moscow, Idaho 83844-2343, USA. E-mail: jshreeve@uidaho.edu; Fax: +1-208-885-5173
bDepartment of Chemistry, Michigan State University, East Lansing, Michigan 48824, USA
First published on 15th October 2024
Historically hydrazine (N2H4) has served an essential function as a fuel in liquid rocket propellants; however, its intrinsic volatility and toxicity pose significant challenges in fulfilling the requirements for environmentally friendly and high-performance propellants. Introducing hydrazine onto a nitrogen-rich framework offers the possibility to use it as solid-rocket propellant. Now for the first time both hydrazine and nitroamine groups, energetic small groups, were introduced onto a tetrazine ring through stepwise functionalization. N-(6-(3,5-Dimethyl-1H-pyrazol-1-yl)-1,2,4,5-tetrazin-3-yl)nitramide (3) serves as an energetic intermediate, which upon reaction with hydrazine or ammonia results in the synthesis of unsymmetrically substituted tetrazine derivatives (4 and 8) via nucleophilic substitution and salt formation (a domino or cascade reaction). Compounds 5 and 9 (salts of 4 and 8, respectively) exhibit detonation properties on a par with RDX, providing the added benefits of high nitrogen content and reduced sensitivity, and 7 and 11 (neutral derivatives of 4 and 8, respectively) show promising propulsive properties, highlighting their potential as solid rocket propellants. This research will significantly advance the synthesis of unsymmetrically substituted tetrazines, enabling precise control over their energetic properties.
Tetrazine, a six-membered heterocyclic ring with four nitrogen atoms, is highly sought after as energetic materials not only because of their nitrogen content but accessibility.24–29 The most prevalent method for preparing symmetric tetrazines involves cyclization of two nitrile molecules to form a 1,4-dihydro-s-tetrazine precursor, which is then typically oxidized using a nitrous reagent. Similarly, symmetric tetrazines can also be obtained through the reaction of 1,2-diketones with hydrazine. Over the years researchers have demonstrated that 3,6-bis(3,5-dimethyl-1H-pyrazol-1-yl)-1,2,4,5-tetrazine (1), obtained from a later method,30 serves as a crucial precursor in the synthesis of nitrogen-rich energetic compounds. Its C3 and C6 sites are highly reactive, which enables straightforward substitution by nucleophiles to yield diverse derivatives (Fig. 1).
While nucleophilic substitution on 3,6-bis(3,5-dimethyl-1H-pyrazol-1-yl)-1,2,4,5-tetrazine is well-documented, exploration of stepwise selective unsymmetric functionalization remains limited.31–36 Previous methods for obtaining compounds such as 3-amino-6-nitroaminotetrazine (ANAT) and N,N′-(1,2,4,5-tetrazine-3,6-diyl)dinitramide involve drawbacks such as requiring high temperatures (140 °C) and pressures (liquid NH3 in a steel vessel) during the synthesis of 1,2,4,5-tetrazine-3,6-diamine (Fig. 2).
Recently, the utility of compound (1) has been demonstrated in the synthesis of fused energetic materials (Fig. 2). A notable strategy involves cyclization reactions between hydrazine (NH2–NH2) and cyanogen bromide to produce triazolo-triazine fused derivatives.37–39 Given the broad range of energetic materials that can be obtained through asymmetric substitution and their potential applications, there is a need for alternate approaches. In this study, we have synthesized new unsymmetric substituted tetrazine derivatives through the stepwise functionalization of 3,6-bis(3,5-dimethyl-1H-pyrazol-1-yl)-1,2,4,5-tetrazine using a straightforward approach. The aim of the method is to identify more advanced energetic compounds with further optimized properties (Fig. 3).
Compound 8 was previously obtained by the reaction of 3-amino-6-nitroaminotetrazine33 (ANAT) with aqueous ammonia (Fig. 2). Here, it was formed by using not only compound 3 and aq. ammonia but with N,N′-(1,2,4,5-tetrazine-3,6-diyl)dinitramide and aq. ammonia (Scheme 1). Salts 9 and 10 were obtained directly from 8 in quantitative yields by taking advantage of their low solubility in water. Compound 8 was neutralized effectively with 10% H2SO4, producing 11 in quantitative yield (Scheme 1). In contrast to compound 4, the reaction of compound 8 with AgNO3 followed by N2H5·Cl results in hydrazinium salt 12. Compound 7 was reacted with gaseous NH3 in ethanol to yield 13.
Single crystals of compound 9 suitable for X-ray analysis were obtained by slow evaporation from methanol:
water (1
:
1) mixtures. It crystallizes in a triclinic (P
) space group with one water molecule in the crystal lattice as 9·H2O. The crystal structure comprises one nitramide anion and one TATOT cation, resulting in the molecular formula C5H9N15O2·H2O, with a density of 1.805 g cm−3 at 100 K (ESI, Section S2†). Notably, the nitrogen and oxygen atoms of the anion form strong hydrogen bonds with the surrounding TATOT cations, forming bonds with lengths ranging from 1.85 Å to 2.47 Å (Fig. 5D–F). In 9·H2O, planar stacking of tetrazine and TATOT rings is also seen (Fig. 5E). The interlayer spacing between the rings is 3.1 Å, indicating strong π–π interactions. The packing index is calculated to be 77.4%. Despite having one water molecule in the crystal lattice, it exhibits good density owing to the planar packing and strong O⋯H/H⋯O and N⋯H/H⋯N bond networks.
Single crystals of compound 11 suitable for X-ray analysis were obtained by slow evaporation from methanol:
water (1
:
1) mixtures. It crystallizes in an orthorhombic (Pbca) space group and is comprised of a tetrazine ring substituted with one amino and one nitroamino group, resulting in the molecular formula C2H3N7O2, with a density of 1.868 g cm−3 at 100 K (ESI, Section S2†). The intermolecular hydrogen bond lengths between molecules range from 2.05 Å to 2.12 Å (Fig. 5G–I). The packing index is calculated to be 76.6%. The packing diagram reveals planar packing with strong O⋯H/H⋯O and N⋯H/H⋯N bond networks, which contribute to high density and good stability.
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Fig. 6 DSC analysis at the heating rate of 5 °C min−1 and 10 °C min−1 (A) 5. (B) 7. (C) 9. (D) 10. (E) 11. (F) 13. |
To study structure–property relationships, in-depth exploration of weak interactions was conducted via Hirshfeld surface and 2D fingerprint analyses.40,41 The red regions on the Hirshfeld surfaces indicate interactions between neighboring molecules. For compound 5, four tiny spikes were observed in the 2D fingerprint plot, representing O⋯H/H⋯O and N⋯H/H⋯N hydrogen bond interactions (Fig. 7B). The total calculated populations of stabilizing O⋯H/H⋯O and N⋯H/H⋯N interactions in compound 5 are 21% and 42%, respectively. The π–π interactions resulting from stacking of the anion and cations can be visualized by displaying non-covalent interaction plots (Fig. 7C).
Similarly for compounds 9·H2O and 11, spikes were observed in the 2D fingerprint plot, representing O⋯H/H⋯O and N⋯H/H⋯N hydrogen bond interactions (Fig. 7E and H). The total sum of calculated populations of O⋯H/H⋯O and N⋯H/H⋯N interactions in compounds 9·H2O and 11 are 58% and 50%, respectively. The π-stacking between rings is visualized by plotting non-covalent interactions plots and are shown in Fig. 7F and I. A large sum of H-bond interactions in combination with π-stacking interactions enhance the thermal stability of compounds 5, 9·H2O and 11.
For compounds 5–13, sensitivities to impact and friction were measured by using BAM standard methods and are given in Table 1. These compounds show acceptable sensitivity towards impact and friction. The sensitivities of compounds 5, 9 and 11 are further explained from both crystal structure and at the molecular level. They have a layer-like packing pattern in the crystal structure, which when subjected to external stimuli can transform the mechanical energy into relative motion between layers. At the molecular level, sensitivities of materials toward impact are very closely related to their electrostatic potentials (ESPs). The electrostatic potentials (ESP) of compounds 5, 7 and 11 were calculated based on the B3LYP/6-311G(d, p) method with optimized structures.42,43 ESP minima and maxima for compounds 5, 7, and 11 are −82, −26, −27 kcal mol−1 and +107, +55, +57 kcal mol−1, respectively (Fig. 8).
T d (°C) | ISb (J) | FSc (N) | ρ (g cm−3) | ΔHfe (kJmol−1) | D v (m s−1) | P (GPa) | I sp | |
---|---|---|---|---|---|---|---|---|
a Temperature (onset at 5 °C min−1) of decomposition. b Sensitivity to impact (IS). c Sensitivity to friction (FS). d Density at 25 °C using gas pycnometer. e Molar enthalpy of formation (calculated using isodesmic reactions with the Gaussian 03 suite of programs (revision D.01)). f Velocity. g Pressure (calculated using EXPLO5 version 7.01.01). h Specific impulse of neat compound calculated with EXPLO5 V 7.01.01 (Isp). i Ref. 44. | ||||||||
5 | 159 | 12 | 240 | 1.74 | 1120.7 | 8846 | 29.4 | 239 |
6 | 162 | 6 | 360 | 1.76 | 671.9 | 8597 | 26.9 | 212 |
7 | 139 | 8 | 120 | 1.75 | 497.6 | 8873 | 31.0 | 253 |
8 | 174 | 10 | 120 | 1.63 | 526.3 | 8713 | 28.6 | 258 |
9 | 241 | 25 | 240 | 1.71 | 1032.5 | 8541 | 27.2 | 236 |
9·H2O | 240 | 25 | 360 | 1.76 | 791.0 | 8810 | 28.9 | 228 |
10 | 252 | 25 | 360 | 1.67 | 584.0 | 7934 | 22.3 | 207 |
11 | 175 | 7 | 160 | 1.82 | 395.1 | 8917 | 32.0 | 245 |
12 | 135 | 8 | 240 | 1.62 | 397.7 | 8494 | 26.2 | 233 |
13 | 123 | 7 | 240 | 1.60 | 205.5 | 8046 | 22.8 | 208 |
RDXi | 204 | 7.5 | 120 | 1.80 | 92.6 | 8795 | 34.9 | 287 |
The densities of 5–13 were measured using a gas pycnometer at ambient temperature under a helium (He) atmosphere and range from 1.60 g cm−3 to 1.82 g cm−3 (Table 1). The enthalpies of formation of the newly synthesized compounds were calculated using the isodesmic method with the Gaussian 03 suite of programs45 giving values for compounds 5–13 in the range from 205.5 to 1120.7 kJ mol−1 (Table 1). All compounds have positive enthalpies of formation owing to the presence of multiple NN bonds. With experimental densities and calculated enthalpies of formation, detonation properties of compounds 5–13 were calculated using EXPLO5 (v7.01.01). The values of calculated detonation velocities and detonation pressures are given in Table 1 and fall between 8046–8917 m s−1 and 22.3–32.0 GPa, respectively, with 11 showing the highest detonation velocity and pressure. The detonation properties of compounds 5 and 11 are comparable to benchmark explosive RDX.44
The colors of the unsymmetrically substituted tetrazine derivatives 3–13 are shown in Fig. 9 and from pink to red to orange. In contrast with most energetic salts, compounds 7 and 11 exhibit very low solubility in water. For 7 and 11, the explosive behavior was determined through a hot needle test, viz., a red-hot (glowing) needle tapped on a 10 mg sample. Both compounds 7 and 11 show a sharp deflagration with a flame (Fig. 9B and C). For 7 and 11, the amount of N2 gas released in the detonation products (calculated from the 7.01.01 version of EXPLO5) is 62% and 61%, respectively, making them environmentally friendly materials (Fig. 9D and E).
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Fig. 9 (A) Colors of compounds 3–13. (B) Hot needle test for 7. (C) Hot needle test for 11. (D) Composition of detonation products for 7 [wt%]. (E) Composition of detonation products for 11 [wt%]. |
Hydrazine has traditionally played a vital role as a fuel in liquid rocket propellants, but its inherent volatility and toxicity present major hurdles in developing eco-friendly and high-performance propellants.46 Consequently, synthesizing tetrazine derivatized with hydrazine allows for leveraging the beneficial properties of hydrazine while minimizing its toxic and volatile nature. To evaluate the applicability of 7 and 11 as solid propellants, their performance was evaluated as monopropellants (neat) and composite propellants.
The specific impulse (Isp) values were calculated using EXPLO5v7.01.01 software at chamber pressure 7 MPa, expansion pressure ratio (Pc/Pe) of 70, initial T of 3500 K, ambient pressure of 0.1 MPa at the equilibrium, and expansion through the nozzle. The Isp values of 7 and 11 as monopropellants (neat) are 253 s and 245 s, respectively, which is higher than AP (157 s) and ADN (206 s). Additionally, the Isp values of four composite propellant formulations using 7, 11 and RDX (i) 88% of compound and 12% Al, (ii) 78% of compound, 12% Al, and 10% HTPB. (iii) 80% compound, 20% AP (iv) 42% compound, 20% AP, 20% HTPB and 18% Al, were calculated and the results are listed in Table 2. The specific impulse values (Isp) of 7 and 11 are comparable to the benchmark explosive RDX.47,48
I sp , [s] | I sp , [s] | I sp , [s] | I sp , [s] | I sp , [s] | |
---|---|---|---|---|---|
a I sp = specific impulse of neat compound (monopropellant). b I sp = specific impulse at 88% compound and 12% Al as fuel additive. c I sp = specific impulse at 78% compound, 12% Al, and 10% HTPB as a binder. d I sp = specific impulse at 80% compound, 20% AP. e I sp = specific impulse at 42% compound, 20% AP, 20% HTPB and 18% Al. f Specific impulse calculated at an isobaric pressure of 70 bar and initial temperature of 3300 K using EXPLO5 V 7.01. | |||||
7 | 253 | 263 | 244 | 260 | 234 |
11 | 245 | 254 | 238 | 255 | 231 |
RDX | 267 | 278 | 259 | 268 | 242 |
Footnote |
† Electronic supplementary information (ESI) available: Synthesis of compounds, isodesmic reactions, characterization data. CCDC 2378050 (5); 2378051 (9·H2O); 2378052 (11). For ESI and crystallographic data in CIF or other electronic format see DOI: https://doi.org/10.1039/d4ta06039c |
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