Page 46 - ITU Journal Future and evolving technologies Volume 2 (2021), Issue 7 – Terahertz communications
P. 46

ITU Journal on Future and Evolving Technologies, Volume 2 (2021), Issue 7





            1                                 1                                1
                                        Total                             Total                            Total
           0.9                          H O  0.9                          H O  0.9                         H O
                                         2                                2                                 2
           0.8                               0.8                               0.8
           0.7                               0.7                               0.7
           Transmittance  0.5               Transmittance  0.5                Transmittance  0.5
           0.6
                                                                               0.6
                                             0.6
           0.4
                                                                               0.4
                                             0.4
           0.3                               0.3                               0.3
           0.2                               0.2                               0.2
           0.1                               0.1                               0.1
            0                                 0                                0
                        0                  1             0                   1             0                   1
                       10                 10            10                  10            10                  10
                        Frequency [THz]                   Frequency [THz]                   Frequency [THz]
                    (a) Altitude = 0 km.              (b) Altitude =16km.              (c) Altitude =35km.
          Fig. 3 – The transmittance of Earth‑space links at several altitudes from one of the driest locations of the Earth, i.e., ALMA, denoting the fraction of EM
                                                           ∘
          radiation after experiencing molecular absorption. The zenith angle is 35 .

          Suen et al. further investigated the performance of a THz   obtain  the  availability  of  the    link  according  to  some
          ground  to  geostationary satellite  links  [16].  They  have   criteria  (e.g.,  Line  of  Sight  (LOS)  and  weather
          shown  that  utilizing  radio  astronomy  platforms  with   conditions).  The analysis in [20] shows that even with a
          large aperture antenna arrays,  which  are  located  at  dry   relatively  high  water  vapor  density,  data  rates  on  the
          sites  of  Earth,  for  satellite  communications  1  terabit/  order of tens of Gbps can be achieved.
          second  link  performance  can  be  exceeded  in  clear
          atmosphere  conditions  [16].  In  [17],  the  authors  show   3.2  Spreading loss
          that  1  terabit/second  is  attainable  in the low THz band
          for  ground/satellite  links  utilizing  massive  antenna   As  an  Electromagnetic  (EM)  wave  propagates  through  a
          arrays  and  establishing  the  ground  stations at Tanggula,   medium  it  expands  and  this  leads  to  a  loss  called  sprea-
          Tibet, where PWV is very low.                        ding   loss.   Spreading   loss   is   one   of   the
                                                               signi icant  challenges  limiting  communication  to  short
          3.1.2   High and low altitude platforms              distances  at  THz  frequencies  because  free  space  path
                                                               loss  increases  with  the  frequency  in  a  quadratic
          To   combat   high   atmospheric   attenuation   in   relation  according  to  Friis’  law.   Regarding   space
          ground/satellite  THz  links,  placing  transceivers  on   links,  we  consider  the  distances  at  least  on  the
          airborne platforms has been proposed in [16, 18].  High   order   of   thousands   of  kilometers.  On  the  other
          and low altitude platforms such as aerostats, aircraft, and   hand,  transmit  power  in  THz  frequencies  is  on  the
          high  altitude  balloons  can  be  employed  for  transceiver   order   of   milliwatts   due   to  immature  THz  source
          placement.   These  platforms  need  a  lower  aperture   technology,  which  is  also  called  the  THz  gap.  Thus,
          diameter  compared  to  ground‑based  transceivers  and   high   gain   antennas   with   high  directivity   are
          can also offer performances comparable to ground‑based   required  for  THz  space  links.   Several  approaches
          platforms with large apertures since they operate at the   for   combating   the   problem   of   high  propagation
          altitudes  where  water  vapor  density  is  low  [16].  In   loss   have   been   proposed   in   the  literature
          Fig.  3,  Earth‑space  link  transmittances  for  various   [21].   Some   of   these   solutions   apply   to  indoor
          altitude  levels  in  a  dry  location  of  Chile,  which  are   and  nano‑scale  communications  such  as intelligent
          simulated  in  the   Planetary   Spectrum   Generator   surfaces  controlling  the  behavior  of  an  EM wave  [22]
          (PSG)  [19],  is  depicted.  According  to  this,  numerous   and  graphene  plasmonic  nano‑antennas  [23].  In   the
          bands,  which  are  not  feasible  to  use  at  sea  level,  are   following   section,   we   discuss   the   potential
          available for use at high altitudes.                 solutions for THz space links.

          3.1.3   Hybrid ground/satellite links                3.2.1   Radio astronomy optics

          Placing  ground  stations  only  at  dry  locations  can  limit   Large  aperture  THz  optics,  which  are  exempli ied  by
          the potential of THz communication.  Akyildiz et al.  pro‑   ALMA   comprising   54   re lector   antennas   with
          pose  ground‑satellite  links  enabled  by  microwave   12  meter  diameter  and  12  smaller  antennas  with  a
          (e.g., X band  (8‑12  GHz),  Ku  band  (12‑18  GHz,  Ka‑band   7  meter  dish diameter,  are  already  being  used  by  radio
          (26.5‑  40  GHz)),  and  mm‑Wave/THz  bands  for  small   astronomy.  In   line   with   this,   one   approach   is
                                                               employing   large  aperture  THz  ground  stations  and
          satellites  called  CubeSats  in  [20].  If  a  ground/satellite
                                                               airborne  stations  with  smaller  apertures  [16].  Large
          link   is   not   suitable   for   transmission   at   THz
                                                               apertures  can  provide  high   gain;   however,   one
          frequencies,  mmWave  and  microwave  bands  can  be
                                                               drawback  is  that  the construction cost increases with
          utilized.  The idea is based on sending a pilot signal to   the diameter [18].

          34                                 © International Telecommunication Union, 2021
   41   42   43   44   45   46   47   48   49   50   51