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pure microporous carbon replica with a surface area as high
2.2. The carbon infiltration processes
2
3
as 3600 m /g and with a micropore volume of 1.5 cm /g.
This concept was applied by Ryoo et al. [9] for the
synthesis of a carbon replica (named CMK-1) with the use
of an ordered mesoporous silica like MCM-48 as template.
Since, numerous carbon replicas have been prepared by
using different mesoporous templates (SBA-15, HMS, etc.)
and carbon precursors. Various carbon-filling techniques
were also tested such as the sucrose solution impregnation
followed by carbonization [9], or the pyrolitic decompo-
sition of propylene gas [10]. To our knowledge, the study of
the characteristics of the carbon replica obtained, for a given
mesoporous template, using different carbon precursors and
preparation route, has not been investigated.
The sucrose process is performed as indicated by Ryoo
et al. [9] and is not reported in details here. Briefly, a liquid
solution of sucrose was mixed with the SBA-15 silica at
room temperature in the presence of H SO (catalyst) before
2 4
to be dried and subsequently impregnated with another
sucrose solution. The mixture was then heat-treated in
vacuum at 1173 K for 3 h. These two liquid-impregnation
steps allow a carbon content of 36 wt% to be reached for the
SiO /C material.
2
The chemical vapor deposition (CVD) process is based
on the pyrolytic decomposition of propylene (2.5 vol% in
Argon) at 1023 K on the SBA-15 silica matrix as reported
elsewhere [10]. The duration of the deposition allows a
In the present work, several carbon materials were
synthesized by means of two different impregnation routes
and three different carbon precursors: the liquid impreg-
nation (with sucrose and pitch) and the gas phase
impregnation with propylene. Pitch is an excellent source
of graphitizable [11,12] carbon, both readily and cheap
since the calcined mesophase formed during the pitch
carbonization generates a pre-graphitic structure that can be
developed into a graphitic one by a high-temperature
treatment. All these infiltrations were performed on the
same batch of SBA-15 silica, an ordered mesoporous silica
with an one dimensional hexagonal arrangement of
mesopores interconnected with micropores. Therefore a 3
D-porosity is present in that host matrix that allows the
cohesion of the carbon replica. The present paper deals with
the comparison of different carbon-infiltrated silicas (SiO2/
C materials) and their corresponding carbon replicas. The
influence of the carbon content was also investigated in
order to get a better insight of the mechanisms of the carbon
filling within the host matrix regarding to the precursors
used. The resulting carbons were characterized using
different techniques and their thermal stability (in inert
atmosphere) was studied. Moreover, it is worth noting that
pitch petroleum was never used as liquid carbon precursor
for the infiltration of ordered mesoporous silica materials.
control of the carbon content in the final SiO
this study, values in the range 22–52 wt% of carbon into the
SiO /C have been obtained, compared to the maximal
/C material. In
2
2
theoretical value of about 63 wt% for the material SBA-15/
C used for this study.
For the Pitch process, petroleum pitch named ‘Ashland
A240’ was used as the carbon precursor. A calculated
amount of pitch (density 1.24) was mixed with the SBA-15
template in order to fill all its mesoporosity (pore volume
0
3
.95 cm /g). The pitch impregnation was performed by
stirring this mixture for 4 h at 575 K (temperature which
corresponds to the lowest viscosity of the pitch). The SBA-
1
5/Pitch mixture was cooled down before to be heat-treated
in argon up to 1175 K (heating rate: 3 K/min) for the
conversion of pitch to carbon. With a pitch having a carbon
yield of 45 wt%, a carbon content of about 36 wt% was
obtained for the SiO /C sample after one-impregnation. A
2
second impregnation was performed on the SiO /C sample
2
assuming that all the pitch all the pitch of the first infiltration
was introduced into the porosity. It allows reaching a carbon
content of 48 wt%.
All the SBA-15/C samples were then treated with
hydrofluoric acid to selectively leach out the silica matrices
and recover the carbon replicas [9]. The host silica SBA-15
template as well as the SBA-15/C and the C samples were
characterized by different techniques as described below.
2
. Experimental
2
.3. Characterizations
2
.1. Synthesis of the mesoporous silica template: SBA-15
The different materials (SiO moulds, SiO /C composites
2
2
and carbon replicas) were characterized by powder X-ray
diffraction (XRD) on a Philips diffractometer (Cu Ka1
radiation (l ¼ 0:15406 nm)). Nitrogen adsorption/desorp-
tion measurements were performed on a Micromeritics
ASAP 2010 at 77 K. Prior to the measurements, the samples
were outgazed at 473 K overnight. The specific surface area
was determined using the BET method in the relative
pressure 0.02–0.2 [13]. The pore volume was calculated by
considering the volume of nitrogen adsorbed at the value of
The synthesis of SBA-15 silica was performed using 1 g
of Pluronic P123 (BASF), 65 g of H O, 9.7 g of 12 M HCl
2
and 2.1 g of tetraethylorthosilicate (TEOS, Fluka, 98%).
The mixture of P123/water/hydrochloric acid was stirred
vigorously before the TEOS addition. This mixture was
aged at 313 K for 24 h followed by a second treatment at
3
50 K for 24 h. After filtration and washing, the powder is
dried at room temperature and heat-treated at 873 K in
air for 6 h to remove the organic template before using it
as a mould.
P=P of 0.95. The mesopore-size distribution was evaluated
0
by the Barett–Joyner–Halenda method from the desorption