| CDC Teams | ||
|---|---|---|
| Team | Responsibilities | Design Disciplines |
Space Segment![]() |
•Payload and spacecraft subsystem design •Top-level ground segment and software sizing •Parametric cost and performance estimation |
Astrodynamics, payload, command and data handling, communications, attitude determination and control, electrical power, propulsion, structure, thermal, ground, software, cost, configuration |
System Architecture
|
•Constellation design and coverage analysis •Vehicle size and launch manifest determination •Concept of operations and ground segment architecture •Analysis of relative cost vs. requirements |
Constellation, payload, spacecraft, availability, ground, cost, utility |
Kinetic Energy Weapons
|
•Payload and spacecraft subsystem design/analysis •Constellation and endgame performance estimation •Parametric system cost analysis |
Configuration, sensor, ordnance, guidance, power, propulsion, structure, ground, carrier vehicle, cost |
Space Maneuver Vehicle
|
•Flexible, fast response, reusable launch vehicle (requires boost vehicle) On-orbit payload support •subsystem design and cost analysis |
Command and data handling, communications, attitude determination and control, electrical power system, propulsion, thermal, ground, software, vehicle configuration, cost |
Ground Systems
|
•Estimation of facilities, personnel, processing, communications, and software •Determination of information, functional, and communication architecture trades |
Information architecture, communications architecture, software, processing, staffing, facilities, spacecraft, cost |
Communications Payload![]() |
•Detailed communications payload subsystem design and trades •Top-level spacecraft estimation •Performance, hardware configuration, and cost estimation |
Link analysis, radio-frequency units, modulation analysis, orbital analysis, digital, coding, laser, spacecraft |