Page 40 - hisdeSAT annual report 2013
P. 40

by INTA. These tests demonstrate the ability of the
                                                          communicating with the Ground Segment developed
                                                          were  started  on the  PAZ  system  by  the  satellite
                                                          Once the satellite was fully integrated, tests

                                                          commenced.
                                                          and functional testing  of the satellite  as a whole
                                                          satellite completed its integration phase in September
                                                          was assembled in the main body of the satellite. The
                                                          very satisfactory results, and after which time each
                                                          tested to measure their radar performance, rendering
                                                          integrated into the three main modules and were
                                                          During  the  first  half  of  the  year,  12  panels  were

                                                          the satellite will be ready for release.
                                                          to conduct the final environmental testing, after which
                                                          of the satellite to the IABG facilities in Munich, in order
                                                          important milestones that culminated in the shipping
                                                          Concerning the PAZ programme, 2013 has seen many

                                                          required by Spanish users.
                                                          end products that meet the performance standards
                                                          with ESA under this programme in order to produce
                                                          Hisdesat continues to work both with CDTI and

                                                          one another.
                                                          satellite and the ground segment communicated with
                                                          was successfully conducted, during which time the
                                                          the end of 2013 the first test of the complete system
                                                          2012 to launching the CDR subsystem in late 2013. At
                                                          preliminary design review (PDR) phase at the end of
                                                          The INGENIO Ground Segment has evolved from the


                                                          carried out throughout the month of October.
                                                          qualification model, the environmental testing was
                                                          following the completion of the integration of the
                                                          their final configuration.  Concerning the Instrument,
                                                          the subsystems, which are already installed and in
                                                          rebuilt and the first tests are being conducted on
                                                          INGENIO flight model platform has been completely
                                                          in the development of the ground segment. The
                                                          2013, both in the manufacture of the satellite and
                                                          INGENIO has continued to achieve milestones during






                                                          OBSERVATION PROGRAMME


                                                          4.3 DEVELOPMENT OF THE






                                                                                                                    © CNES 2007
   35   36   37   38   39   40   41   42   43   44   45