Page 220 - Intro to Space Sciences Spacecraft Applications
P. 220

Spacecraft Design
                                                                                    207
                        This phase has a duration of from one to two years. The costs associat-
                      ed with this study are usually four to eight percent of total mission costs.

                                                              many
                                                            In
                      DesigdDevelopment Phase (Phase 0). instances, these phas-
                      es are combined into a  single phase,  since by  now  the commitment to
                      build  the  system  may  already  have  been  made.  The  purpose  of  the
                      designldevelopment phase is the implementation of the Phase B Plan. The
                      final design, production development, and fabrication of  hardware and
                      software needed to translate the mission into a reality begins. The phase
                      often  includes  launch,  deployment,  and  postlaunch  on-station  system
                      checkouts  and  follow-on  operations.  Depending  on  the  scope  of  the
                      deployed  system  (Le.,  multiple  satellite weather  or  navigation  system
                      developments versus one-of-a-kind single satellite programs) this phase
                      can have an extremely variable duration, lasting from two years to more
                      than a decade. The costs associated with this phase can also vary consid-
                      erably-from  tens of millions of dollars for SMALLSAT or LIGHTSAT
                      missions to billions of  dollars for defense or planetary exploration satel-
                      lite programs.
                        Key activity categories during this phase are linked to the scheduled
                      sequence of events, with each item listed below applicable to all the mis-
                      sion elements (space and ground systems and subsystems; payload ele-
                      ments including spacecraft/payload/ground system interfaces and links):
                        1. Design and development.
                        2. Fabrication.
                        3. Assembly.
                        4. Integration.
                        5. Test and evaluation (ambient and space environment exposures).
                        6. Transfer to the launch site followed by mating and prelaunch checkout.
                        7. Launch and launch sequence monitoring.
                        8. On-orbit checkout.
                        9. Postlaunch  operations,  which  can  include  retrieval  and  on-orbit
                          change or repair.

                        Perhaps the most important milestones in the Phase C/D process, shown
                      in Figure 9-2, are the preliminary design review and the critical design
                      review (PDR and CDR). These signify the release of the design for final
                      production review (in the PDR), and the essential freeze of the design for
                      fabrication and assembly (in the CDR).
   215   216   217   218   219   220   221   222   223   224   225