The morphology characteristics and crystalline structures of samples are determined. As shown in
Fig. 1a, the length and width of MIL-88A(Fe) nanorods with smooth and dense surface are about 2 µm and 500 nm, respectively. After surface modification and etching of MIL-88A(Fe), the hollow capsule shell-shaped MIL-88A(Fe)/P
2W
18 composite can be obtained (Fig. S1a in Supporting information). In Fig. S2 (Supporting information), it can be observed from Fourier transform infrared spectroscopy (FTIR) that the main peak position of MIL-88A(Fe) do not change significantly after being modified by P
2W
18, demonstrating that the structure of MIL-88A(Fe) template is not destroyed after etching. The characteristic peaks of W−O group (910, 943, and 1075 cm
−1) can be clearly observed from MIL-88A(Fe)/P
2W
18, which confirms that P
2W
18 is modified on the surface of MIL-88A(Fe) shell. In order to detect the crystal structure and phase purity, X-ray diffraction (XRD) analysis of MIL-88A(Fe), P
2W
18, and MIL-88A(Fe)/P
2W
18 is performed (Fig. S3 in Supporting information). As observed, the diffraction peaks of MIL-88A(Fe) are identical with the data published in references [
42], suggesting that a relatively pure MIL-88A(Fe) template. For MIL-88A(Fe)/P
2W
18, the characteristic diffraction peaks of P
2W
18 are clearly displayed, which further illustrates that P
2W
18 is successfully modified on MIL-88A(Fe). Moreover, the loading amount of P
2W
18 is calculated to be 30.25 wt%
via inductively coupled plasma optical emission spectrometer (ICP-OES) (Table S1 in Supporting information). Subsequently, MIL-88A(Fe)/P
2W
18 composites are carbonized at 300, 400, 500, and 600 ℃. Due to the insufficient carbonization at 300 ℃, one can see from the XRD patterns (
Fig. 1b) that there are no obvious changes compared with MIL-88A(Fe)/P
2W
18, and the resulting material can be marked as MIL-88A(Fe)/P
2W
18–300. When the calcination temperature is 400 ℃, the diffraction peaks of P
2W
18 and Fe
3O
4 can be clearly observed (marked as C-Fe
3O
4/P
2W
18). The peaks at 6.44°, 9.35°, 24.69°, 25.38°, 27.35°, 29.07°, and 35.93° correspond to the index numbers of P
2W
18 (100), (−111), (223), (204), (115), (−404), and (−307), respectively. Meanwhile, diffraction peaks at 18.27°, 30.09°, 35.42°, 43.05°, 53.39°, 56.94°, and 62.52° correspond to the index numbers of Fe
3O
4 (110), (220), (311), (400), (422), (511) and (440), respectively. Furthermore, as shown in Fig. S4 (Supporting information), the characteristic peaks of MIL-88A(Fe) cannot be found from FTIR of C-Fe
3O
4/P
2W
18, suggesting the sufficient carbonization of MIL-88A(Fe) at 400 ℃. Fig. S5 exhibits that the content of C in C-Fe
3O
4/P
2W
18 composite is calculated to be 6.8 wt%. When the temperature continues to rise to 500 ℃ and 600 ℃ (
Fig. 1c), no diffraction peaks of P
2W
18 are observed due to the higher carbonization temperature, and the diffraction peaks of FeWO
4 are existent, which indicates the disintegration of P
2W
18, thus the obtained materials are marked as C/FeWO
4-500 and C/FeWO
4-600, respectively. Furthermore, MIL-88A(Fe)/P
2W
18-300 and C-Fe
3O
4/P
2W
18 maintain the original hollow capsule shell structure with uniform distribution (
Fig. 1d and Fig. S1b in Supporting information). With the temperature increasing, the surface of C/FeWO
4-500 is slightly fragmented, and the framework of C/FeWO
4-600 is completely fractured and collapsed (Figs. S1c and d in Supporting information). Based on the points discussed above, C-Fe
3O
4/P
2W
18 presents the optimizational carbonization and retains the original hollow capsule shell structure. When employed as the sulfur host, C-Fe
3O
4/P
2W
18 hollow capsule can relieve the volume change of sulfur cathode and achieve high sulfur loading. The high resolution transmission electron microscopy (HRTEM) images in
Fig. 1d demonstrate that the lattice fringe spacings of 0.38 nm and 0.25 nm agree well with (001) plane of P
2W
18 and (311) plane of Fe
3O
4, which proves the high crystallinity of P
2W
18 and Fe
3O
4. Moreover, the elemental mapping and energy-dispersive X-ray spectroscopy (EDX) of C-Fe
3O
4/P
2W
18 show that Fe, O, P, and W elements are uniformly distributed in the shell layer (
Figs. 1e–i).