Page 218 - Intro to Space Sciences Spacecraft Applications
P. 218

205
                                                                Spacecraft Design
                     mission and payload, a number of different concepts may be formulated
                     that  can  achieve  the  mission  objectives,  and  these  concepts  will  be
                     expanded to determine the feasibility of conducting the mission. This con-
                     cept development will include ground system and operations as well as
                     launch vehicle and spacecraft descriptions, but the level of detail is usual-
                     ly in the form of estimates based on contemporary systems and technolo-
                     gies. After the concept is formulated, a rough order ofmagnitude (ROM)
                     cost for the mission is attained using heritage cost models and known
                     costs for subsystems and services. Exceptions to this are unique, one-of-
                     a-kind designs or pioneering first efforts.
                       The results of this phase are reviewed at a “local” level-within  a tech-
                     nical center, military or industrial laboratory, university, or similar orga-
                     nization-to  determine if the concept warrants further consideration out-
                     side  the  group.  For  example,  within  NASA,  if  the  concept  looks
                     promising, an announcement ofopportunity (AO) may be issued which is
                     the first step in defining and selecting the instruments/experiments that
                     will fly on the mission if  it is fully developed and launched. If  concept
                     study results prove to be promising, the evolving program moves on to the
                     next step in Phase A, a more detailed mission evaluation.

                     Mission Analysis Phase (Phase A).  The purpose of the mission analysis
                     phase is to translate the broad mission concepts and objectives into a fea-
                     sible preliminary system design. This is a refinement and expansion of the
                     conceptual study phase made with the intention of providing a concise,
                     clear overview of the proposed system. Implementation planning is done
                     in  cooperation  with  discipline  engineering  groups  (attitude  control,
                     power, thermal, and other spacecraft subsystems areas defined in the pre-
                     ceding chapter), payload specialists (e.g., remote sensors and communi-
                     cations  transponders),  and  ground  and  launch  services  organizations.
                     Financial  analysts  utilize  parametric  cost  models  to  derive  top-level
                     resource estimates for the overall mission and its component elements.
                       Key activities during this phase are system and subsystem trade studies,
                     analyses of performance requirements, identification of advanced technol-
                     ogyAong lead items, risk assessments, and end-to-end  system life-cycle
                     costs as a trade parameter. In addition, considerable attention is given to
                     schedule options and selection and evaluation of operational concepts.
                       Specific tasks to support this phase may  include technical feasibility
                     and  risk  assessments  associated  with  cost  estimate  modeling.  Special
                     attention  is  given  to  interface  identification,  definition,  and  analysis
   213   214   215   216   217   218   219   220   221   222   223