Overview of The Aerospace Corporation’s Concept Design Center Daniel Nigg, Director Concept Design Center Architecture & Design Subdivision
Systems Engineering Division The Aerospace Corporation 16 December 2010 Copyright © 2010 The Aerospace Corporation
The Aerospace Corporation Assuring Mission Success
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Operates a Federally Funded Research & Development Center (FFRDC) that provides scientific and engineering support for launch, space, and related ground systems – Specialized facilities and continuity of effort required for programs that often take decades to complete – End-to-end involvement reduces development risks and costs, and allows for a high probability of mission success
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Corporate core competencies include – Launch certification – System-of-systems engineering – Systems development and acquisition – Process implementation – Technology application
The Concept Design Center (CDC) is one capability frequently used to address the majority of these core competencies
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Why is concept design important? Though space is vast, there’s no room for error
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Early programmatic decision making
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Cumulative % of Budget
– Rapid yet thorough tradespace exploration of new concepts and block upgrades provides better insight into system needs – Identify drivers – Determine feasibility Life Cycle Cost Determination – Assess margins and risks – Identify technology on-ramps – Refine and validate requirements – Identify alternatives and improvements Cost Reduction Opportunities – Path pruning
Proposal analysis and source selection – Define government reference architecture – Provide technical inputs to cost estimation
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Establishing future ETG reachback
Program Phase
– Milestone decision support (PDR, CDR, etc.) – Technology readiness assessments – Program redirection Of all decisions affecting life cycle costs, approximately 70% are made during Concept Design
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CDC Capabilities Bringing customers and technical experts together
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The CDC provides answers to the unique challenge of system conceptualization through effective collaboration in order to design and evaluate space and ground systems in real time
Current investigations involve various teams focusing on technical solutions – Systems Architecture Team (SAT) – Space Segment Team (SST) – Ground Segment Team (GST) – Electo-Optical Payload Team (EOPT) – Communications Payload Team (CPT)
Design Scope
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Utility Definition Concept Design Preliminary Design Critical Design
SAT SST & GST CPT & EOPT
Level of Detail
The CDC has been a Corporate resource serving both the National Security Space and Civil Space communities since its inception in the mid-1990s
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Who uses the CDC? A variety of customers and missions – each with unique requirements
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Primary customers include the Space and Missile Systems Center of Air Force Space Command and the National Reconnaissance Office
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Additional support is provided to – National Oceanic & Atmospheric Administration (NOAA) – National Aeronautics & Space Administration (NASA) – Air Force Research Laboratory (AFRL) – Naval Research Laboratory (NRL)
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GST EOPT
SST Notable programs supported include – Communications/Navigation Outage Forecasting System (C/NOFS) – NAVSTAR Global Positioning System (GPS) – Evolved Expendable Launch Vehicle (EELV) – Geostationary Operational Environmental Satellite (GOES)
Approximately 300 CDC studies completed (1997-2010)
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CPT SAT
CDC Pillars Success built on experience and lessons learned Teams leverage the full breadth and depth of required expertise available – Experience across many programs – Can include regional site experts as needed – 26 average years of experience since bachelor degree
Facilities promote interaction and connection with technical staff and customers – Support for communications and data exchange – Workstations, servers, networks, video projection, audio/video teleconferencing
Processes integrate team & design tools to produce quality results quickly Proven, repeatable, and consistent results by calling on many of the same subject matter experts and integrating the tools they use to support programs well beyond Concept Design
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Multidisciplinary CDC Teams … and their interactions
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System Architecture Team (SAT) – Constellation design and coverage analysis – Top-level element sizing and interface definition – Relative cost versus requirements and utility
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Space Segment Team (SST) – Payload and spacecraft subsystem design – Detailed cost and performance estimation – Top-level ground segment and software sizing
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Ground Segment Team (GST) – Facilities, personnel, processing, communications, and cost estimates – Top-level space segment sizing
Systems Architecture Team
Software
Space Electro-Optical Payload Team (EOPT) & Segment Team Communications Payload Team (CPT) – Detailed payload subsystem trades – Performance and cost estimation – Mission requirements implications – Top-level spacecraft and ground segment estimation
Cost
Customer
Risk
Payload Processing
Core team members for each study plus additional unique expertise as required
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Payload Systems Teams
Ground Segment Team
Organization Teams are staffed from the ETG Matrix ENGINEERING AND TECHNOLOGY GROUP >1300 Engineers & Scientists
SYSTEMS PLANNING SPACE SYSTEMS Electronics & Sensors
SPACE LAUNCH
GROUND SYSTEMS
COMMUNICATION
SYSTEM INTEGRATION DEVELOPMENTAL PLANNING
ADVANCED TECHNOLOGY CIVIL & COMMERCIAL
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Digital & Integrated Circuit Electronics
Communications & Networking
Vehicle Systems
Systems Engineering
Laboratory Operations
Computers & Software
Digital Communication Implementation
Control Analysis
Astrodynamics
Electronics
Electromechanical Control
Performance Modeling & Analysis
Propulsion
Computer Systems Research
Materials
Ground Systems
Communication Electronics
Flight Software Validation
Space Environment
Antenna Systems
Guidance Analysis
Navigation & Geopositioning Systems
Advanced Information Systems Technology
Space Electronics Vulnerability
Communication Architectures
Fluid Mechanics
Radar & Signal Systems
Communication Systems Engineering
Spacecraft Thermal
Mission Analysis & Operations
Flight Mechanics
Space Architecture
Electronics & Power Systems Parts, Materials, & Processes
Electro-Optical Device Evaluation Visible & Infrared Sensor Systems Imagery Products & Exploitation Exploitation, Phenomenology, & Analysis
Network Systems Communication & Signal Analysis
Propulsion
Environments, Test, & Assessment Structural Dynamics Structures Mechanical Systems
Modeling & Simulation
Systems Performance, Estimation, & Algorithms Concept Design Center Cost, Schedule, & Requirements
Mission Oriented Research Special Sensor Fabrication
Information Assurance Technology
Remote Sensing Signatures
Software Assurance
MEMS
Engineering Applications
Vehicle Concepts
Telemetry & Hardware Technology
Engineering Data Systems Product & Process Assurance
Digital Electronics & Electromagnets
Economic & Market Analysis
Acquisition Risk & Reliability Engineering
Advanced Sensor Engineering
Systems Architecture, Engineering, & Cost
Ground Systems Infrastructure Development
Reliability & Statistics
System Delivery & Operations
Software Architecture & Engineering Software Systems Analysis Software Acquisition & Process
Software Systems Engineering
CDC Investigations SST Examples New Concepts & Block Changes Payload Concept
Spacecraft Bus Concept
Parametric Trade Studies
Technology Insertion 10000 Payload
Concept Assessment
Launch 10000 Performance to GTO
8000
8000
6000
6000
Contractor Concept
Data for Costing
Feasibility Alternatives Improvements Margins . . .
Proposal Analysis
Design Information Payload
Propellant
4000 2000
Advanced Technology
Bus
0
4000
Propellant
2000 Bus 0
Program or Other Cost Group
Adaptable application of expert knowledge, tools, and processes
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Proposal #1
Proposal #2
IDEA tool facilitates the process Integrated Data Exchange Architecture
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Subsystem designers’ workbooks exchange data through server Subsystem interfaces are well-defined Design and analysis tools are independent of the underlying SQL database Standard network communications architecture Design Data Server
Database TCP/IP Different mix of technical experts, depending on team needs
Client
Client
Client
Client
ODBC Driver
ODBC Driver
ODBC Driver
ODBC Driver
Design/Analysis Tool
Design/Analysis Tool
Design/Analysis Tool
Design/Analysis Tool
Astrodynamics
Power
Thermal
Structures, ADACS, Comm, Cost, Utility, etc., as needed
Customers, subject matter experts, & database do not need to be co-located
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Distributed Concurrent Engineering Networks link multiple design centers in real-time
Collaboration with Other Candidate Design Center(s) Operations Expertise
Technology Roadmaps & Experimental Mission Expertise
Specific Customer Familiarity & Mission Expertise
Core Teams with CDC Experience, Specific Customer Familiarity, & Mission Expertise
Strengthening customer and collaborator relationships regardless of geographic location
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Concurrent Program Definition Environment Adding expanded context to the technical product Software
Customer Inputs Performance Requirements Optical Aperture Data Collection Rates Onboard Processing Power Modes Data Volume Data Latency Data Downlink Rates Comm Bandwidth & Power Pointing Accuracy Pointing Knowledge Mission Requirements Constellation Size Orbit(s) Mission Lifetime SV Design Life Survivability Radiation Maneuvers Availability Replenishment Design Constraints Tech Freeze Launch Vehicle
CPDE
Cost Risk
Payload Processing Space Segment Team
Subsystem Mass & Power Estimates, Growth Contingencies, SV Dry Mass, Mission delta-V, Propellant Mass, EOL Power, BOL Power (Solar Array & Battery sizing), Thermal Cycling, Technology Readiness, Design Heritage, Comm Availabilities & Durations, Inertias, Deployed & Stowed Packaging, LV Margin, SLOC, Facilities, Personnel, Life Cycle Costs (Dev, Prod, O&M)
Acquisition Strategy Blocks, Spirals Contracting Down-Selection CONOPS Operational Views Performance Capacity Quality Utility Availability Schedule Milestones Tech On- & Off-Ramps Software Management Strategy Funding Budget Profile Risk Identification Mitigation
Incorporates programmatic assessments through feed back into technical team sessions
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CDC Events Timeline Typical for studies with new or repeat customers
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Study Planning (2 to 8 weeks)* – – – –
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CDC design session (2 to 4 half-days)* – – – –
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Customer and CDC systems engineer scope the study Generate Statement of Work (SOW) Tool Development and Research Pre-Session Design/Analysis Work • Subset of the team & customer meet to work specific issues
Mission and customer introduction Customer describes mission goals, needs, wants, and desires Team gathers information from the customer Concurrent design process
Post-CDC session activities (4 weeks)* – Comprehensive report – Contributions by each team member and customer – Detailed assumptions including risk areas and technical considerations
* Timeline assumes minimal tool development & focused study objectives
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Types of Success in the CDC Continuing effort to improve and expand these capabilities
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Design Validation – CDC design validated contractor design very close to what will fly Requirements Validation – Rapid exploration of configurations provided better insight into system needs; requirements rewritten to be unambiguous and verifiable Technical Improvements – Optimized constellations and replenishment strategies to save costs – Developed alternate SV transfer orbit designs, increasing available SV mass for payloads or propellant Cost Reduction – Careful orbit selection to optimize SV duty cycle and power sizing reduced the initial estimated SV mass, allowing spacecraft to fly on smaller launch vehicle Path Pruning – Vetting unfeasible ideas early, saving program cost that would be needed to explore or develop them Team Building – Accelerated customer education – early-on, program personnel are still learning about their system-to-be, and will carry early knowledge and decisions with them – Sharpen skills for other activities such as source selection or cost estimation
Concurrent design provides our customers with timely, integrated, lower risk solutions
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Summary Flexible capabilities for conceptual design
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The CDC – Serves the entire NSS community – Provides insight into the performance, cost, & risk of requirements – Addresses space system architecture, spacecraft, ground systems, and payload concepts – Supports key programmatic decisions by providing sound unbiased technical information throughout program development • Advanced planning, trade studies, cost estimates • RFP preparation, source selection • Milestone decision support, program redirection
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CDC studies can be a gateway into the rest of The Aerospace Corporation – Technical reach-back to entire engineering matrix and toolset – Significant cross-program knowledge base and experience – Adaptable framework supporting design and development activities
Real-time, collaborative, concurrent engineering in Concept Design enables our customers to make informed decisions
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Continued success Built on lessons learned
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The CDC’s real-time, collaborative, concurrent engineering – Is a capability used to rapidly explore the impacts of mission and design requirements on a system
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To enable the design of new concepts or block changes and assessment of proposed designs (in terms of feasibility, alternatives, improvements, margins, etc.) Determine implications of technology insertion Provide technical data for program cost estimation efforts Identify and characterize risks early in a program’s lifecycle
– Requires the right mix of
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Suitable facilities and infrastructure Evolving processes and tools (including standardization and configuration control) Experienced (yet adaptable) subject matter experts with organizational reach-back and support Regular interaction and solicitation of feedback from customers, team members, and their management to direct development of future capabilities
CDC and Corporate leadership are active in the “Concurrent Engineering” community
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Overview of The Aerospace Corporation’s Concept Design Center Daniel Nigg, Director Concept Design Center Architecture & Design Subdivision
Systems Engineering Division 16 December 2010