Scientist, science team members, and equivalent personnel for technology demonstrations are included.
Specific responsibilities include defining the science or demonstration requirements; ensuring the
integration of these requirements with the payloads, spacecraft, ground systems, and mission
operations; providing the algorithms for data processing and analyses; and performing data analysis and
archiving. This element excludes hardware and software for onboard science investigative
instruments/payloads.
Element 05 - Payload: This element includes the special-purpose equipment and normal equipment,
e.g., Ground Support Equipment (GSE), integral to the spacecraft. This includes managing, and
implementing the hardware and software payloads that perform the scientific experimental and data-
gathering functions on board the spacecraft, as well as the technology demonstration for the mission.
Element 06 - Spacecraft(s): The spacecraft that serves as the platform for carrying payload(s),
instrument(s), humans, and other mission-oriented equipment in space to the mission destination(s) to
achieve the mission objectives. The spacecraft may be a single spacecraft or multiple
spacecraft/modules (e.g., cruise stage, orbiter, lander, or rover modules). Each spacecraft/module of the
system includes the following subsystems, as appropriate: Crew, Power, Command & Data Handling,
Telecommunications, Mechanical, Thermal, Propulsion, Guidance Navigation and Control, Wiring
Harness, and Flight Software. This element also includes all design, development, production,
assembly, test efforts, and associated GSE to deliver the completed system for integration with the
launch vehicle and payload. This element does not include integration and test with payloads and other
project systems.
Element 07 - Mission Operations System: The management of the development and implementation
of personnel, procedures, documentation, and training required to conduct mission operations. This
element includes tracking, commanding, receiving/processing telemetry, analyses of system status,
trajectory analysis, orbit determination, maneuver analysis, target body orbit/ephemeris updates, and
disposal of remaining end-of-mission resources. The same WBS structure is used for Phase E Mission
Operation Systems but with inactive elements defined as "not applicable." However, different accounts
must be used for Phase E due to NASA cost reporting requirements. This element does not include
integration and test with the other project systems.
Element 08 - Launch Vehicle / Services: The management and implementation of activities required
to place the spacecraft directly into its operational environment, or on a trajectory towards its intended
target. This element includes launch vehicle, launch vehicle integration, launch operations, any other
associated launch services, and associated ground support equipment. This element does not include the
integration and test with the other project systems.
Element 09 - Ground System(s): The complex of equipment, hardware, software, networks, and
mission-unique facilities required to conduct mission operations of the spacecraft systems and
payloads. This complex includes the computers, communications, operating systems, and networking
equipment needed to interconnect and host the Mission Operations software. This element includes the
design, development, implementation, integration, test, and the associated support equipment of the
ground system, including the hardware and software needed for processing, archiving, and distributing
telemetry and radiometric data and for commanding the spacecraft. Also includes the use and
maintenance of the project test beds and project-owned facilities. This element does not include
integration and test with the other project systems and conducting mission operations.
NASA Work Breakdown Structure (WBS) Handbook Page 56