THIS ANNEX, INCLUDES THE
COVER, CONSISTS OF 4 PAGESThe WBS shall be structured in such a way that it is directly traceable to the Offeror's cost accounting system. The Offeror shall use MIL-STD-881B as a guide. The content shall include, but is not limited to, the following information. The structure of this information does not connote the desired format of the WBS; the Offeror is encouraged to organize the WBS in an innovative fashion that provides the optimum management structure of the program.

A. PROGRAM MANAGEMENT
The program management element refers to business and administrative planning, organizing, directing, coordinating, integrating, controlling, and approval actions designated to accomplish overall program objectives which are not associated with specific hardware items and are not included in systems engineering. Examples of these activities are system level - acquisition management, data management, cost/schedule/performance management, contract and subcontract management, production management, and logistics support

B. SYSTEMS ENGINEERING
The Systems Engineering element refers to the efforts of planning, directing and controlling a totally integrated engineering effort for the system. This item includes, but is not limited to, design engineering, specialty engineering, production engineering, configuration management, system security, system safety, range safety, hazardous materials management, and logistics support analysis. It includes the system engineering activities necessary to integrate the subsystems, as applicable, into a complete end item. The design and production engineering related to the subsystems or components is included with that subsystem or component.

C. RISK REDUCTION DEMONSTRATIONS
The risk reduction demonstrations element refers to the planning and conducting of demonstrations and trade analysis to reduce the risk of the overall program. These demonstrations include but are not limited to demonstrations of state-of-the-art technologies, novel engineering approaches, new processes, and models. Trade analysis will encompass design and associated process capability analysis. The Offeror will identify performance measures, critical design characteristics to meet performance, and critical processes required to meet the design.

D. PAYLOAD MISSION ANALYSIS
The payload mission analysis element refers to the effort required to establish and implement integration requirements to unite Government provided payloads with the launch system to achieve the specified orbit. Included are those activities required to assure successful design and operation of all interfaces. Interface design and mission design activities are included.

E. SYSTEM TEST & EVALUATION
The system test and evaluation element refers to the use of prototype, production, or specially fabricated hardware/software to obtain or validate engineering data on the performance of the system during the development phase. This item includes the detailed planning, conduct, support, data reduction and reports for such testing. It also includes all effort associated with the design and production of models, specimens, fixtures and instrumentation in support of the system level test program. Test articles which are complete units (i.e. functionally configured per the system specs) are excluded. All formal and informal testing up through the subsystem level which can be associated with the hardware/software element are excluded. Acceptance testing is also excluded. These excluded efforts are to be included with the appropriate hardware or software elements.

F. LAUNCH VEHICLE
The launch vehicle element refers to the flight hardware and software required to insert the Government furnished payload into the proper orbit. This element includes, but is not limited to, design, development, production, integration, test, delivery, and support of flight hardware and software. The unique payload mission peculiar hardware and software, that is not provided by the payload manufacturer, is also included.

G. GROUND COMMAND, CONTROL, COMMUNICATIONS AND MISSION EQUIPMENT (GC3ME)
The GC3ME element includes the non-recurring effort required to design, develop, test, produce, and deliver the ground hardware and software for communications, monitoring, and ground control between the launch vehicle/space vehicle and ground processing stations. Effort required to modify these systems is included in this element. It includes all sensors, telemetry, tracking, and control, external communications, data processing equipment, automated launch processing equipment, software, and auxiliary equipment required for conducting EELV system mission planning, launch processing, health management, launch operations, and flight operations.

H. SUPPORT EQUIPMENT
The support equipment element includes all efforts required to design, develop, test, produce, and provide initial delivery of all new or replacement peculiar and common support equipment (including hardware and software) required to operate, support, and maintain the EELV program. This element also includes the software support environment(s) necessary to support the deliverable software post-deployment. It includes all support equipment for mission planning, launch vehicle integration, payload integration, mission element integration, launch operations, flight operations, recovery operations (if applicable), reusable hardware refurbishment (if applicable), readiness, maintenance, and logistics support. Support Equipment includes all test and measurement equipment, support and handling equipment, and software and tools required to fuel, transport, hoist, repair, assemble, test, or inspect EELV hardware.

I. OPERATIONAL SITE ACTIVATION
The operational site activation element refers to the construction, conversion, or expansion of roadways, real estate, utilities, and buildings/facilities required to house, service, process, launch, and support flight hardware/software. Also included are any efforts due to environmental concerns or laws regarding impacts to the human, ecological, or biospherical environment. It also includes installation design, system assembly, installation and checkout, ground system tests, pathfinder operations, and integrated system tests for ground command, control, communications and mission equipment/software, and support equipment/software.

J. FLIGHT SUPPORT OPERATIONS & SERVICES
The flight support operations and services element refers to the activities at the launch and operations sites required to receive, inspect, store, process, mate the payload, checkout, monitor, test, launch, control, track, recover (if applicable), and logistically support the EELV system. Logistics support includes inventory control, purchasing, replenishment spares and repair parts provisioning, consumables supply, launch vehicle maintenance, software maintenance, parts repair/refurbishment, parts cleaning, packaging, handling, storage, transportation, Core Automated Maintenance System (CAMS), Standard Base Supply System (SBSS), waste disposal, and training. It also refers to the maintenance and refurbishment of the facilities and equipment (GC3ME and Support Equipment) at the launch base required during the life of the system.

K. DATA
The data element refers to all deliverable data required to be listed on a Contract Data Requirements List, DD Form 1423. The effort required for initial generation of the data is allocated to the WBS item for which it was created. Included is the assembly, reproduction, packaging, shipping, and storage of the data. Also included is the effort for transforming into Government format with reproduction and shipment if the data is identical to that used by the Contractor, but in a different format.

L. INDUSTRIAL FACILITIES
Industrial facilities refers to the construction, conversion, or expansion of industrial facilities for production, inventory, and Contractor depot maintenance required when that service is for the specific system. This includes, for example, equipment acquisition or modernization, where applicable, and maintenance of these facilities or equipment. This also includes industrial facilities for hazardous waste management to satisfy environmental standards.

M. INITIAL SPARES AND REPAIR PARTS
Initial spares and repair parts include the deliverable spare components, assemblies, and subassemblies used for initial replacement purposes in the materiel system equipment end item. This includes the repairable spares and repair parts required as initial storage to support and maintain newly fielded systems or subsystems during the initial phase of service, at all levels of maintenance and support.

N. INSURANCE/PERFORMANCE INCENTIVE
This includes such elements as reflight insurance, performance incentives, mission success incentives, subcontractor incentives and fees, and Failure Liability Indemnification Plan (FLIP).