integrity engineering-2

Capture the maximum value of your team

Engineering excep6onal aerospace outcomes

Mission Statement

“As the engineering and design partner of

choice, we will enable our clients to optimize

project performance by applying our high end

technical talent to deliver engineering solutions.

Our personnel’s expertise reflects comprehensive

capabilities and broad industry experience that

will be employed in a timely, agile and extremely

cost competitive manner.”

Classifica0on

Small Minority Owned/Disadvantaged Business Cage Code: 3DHZ5 Primary NAICS Codes

541712 Research and Development 541330 Engineering Services 423690 Other Electronic Parts & Equipment Wholesale

Manufactures 541511 Custom Computer Programming Services 561910 Packaging & Labeling Services (Customized Tool

Kits)

Core Competencies

Program/Project Management Subcontract Management

Systems Engineering Aviation Systems Hardware Design

Reverse Engineering

FlexInterface Project Fulfillment™

Integrity’s innova0ve project methodology Interface at any stage or step* of the product development process

(* Over 160 steps iden0fied within the LEAN Process)

•  Defini0on of Requirements (26 step process)

•  Preliminary Design (36 step process)

•  Detailed Design (73 step process)

•  Build and Test (20 step process)

•  Documenta0on (7step process)


Defini0on of Requirements

Preliminary Design

Detailed Design

Prototype Build

Characterize and Test

Produc0on Ready

Documenta0on

System Requirement Review (SRR)

Preliminary Design Review (PDR)

Detailed Design Review (DDR)

Technical Data Package (TDP)

Test Data Review (TDR)

Produc0on Readiness Review (PRR)

Customer Deliverables

FlexInterface Advantage

•  Maintain greater visibility throughout your design cycle •  Address each level of involvement required •  Expedite transi0on 0mes between development stages •  An0cipate and avoid process complica0ons

•  Specialized exper0se and competency – selected for the culture

•  Direct interface with suppliers

•  Senior level supervision (Project Management)

•  Up to MRL 7 product level standards

•  Proven performance

A truly collabora,ve workflow from ini,a,on to comple,on!

Process Op0miza0on

A1tude of Ownership

Addi9onal layer of Senior program oversight

•  Iden0fy poten0al manufacturing improvements

•  Implement innova0ons to reduce fabrica0on and assembly costs

•  Coordinate suppliers to capture opportuni0es for 0me and cost

gains

•  Reduce lifecycle costs and obsolescence risks

Program Management

Program Management •  Project Leadership •  Technical Lead and Direc0on •  Cost and Schedule Management (Earned Value System) •  Hardware and So\ware systems •  Risk and Opportunity Management •  Contract Management •  Engineering Change Management •  Subcontract Management •  Supply Chain Management

•  Supplier and vendor management •  Counterfeit Parts Management •  Purchasing •  Parts planning

•  RFP and Proposal Development and Management •  Product market value analysis

Logis0cs

•  Life Cycle Logis0cs support to US Air Force and Navy Customers and their Prime Contractors

•  Align and refine product support package (product support elements) and sustainment processes to achieve sustainment metrics

•  Op0mize or reduce the logis0cs demand (including the logis0cs footprint) and support processes (training, technical data, supply chain, maintenance, etc.) based on actual condi0ons

•  Develop inventory management strategy and tools for Government Furnished Material and Contractor Furnished Material.

•  Coordina0ng and resolving data interface and security classifica0on issues across the en0re supply chain.

•  Projects •  F4, F16 Mul0na0onal Fighters, U2, and SR71 •  Consolidated Afloat Network Enterprise Services , Liboral Combat Ship

Systems Engineering

•  Comprehensive Test Engineering, TEMP, Test Plans, procedure, scripts development •  Lead for Honeywell’s PDU Subsystem Orion Special Test Equipment

•  Design, build, test ; Na0onal Instruments Test Suite Experience; Labview

•  Systems Life Cycle Process, Requirements Development, Management, SEMP –  DOORS, Ra0onal Tool Set (ReqPro)

•  CONOPS development, Customer CONOPS, ORD, TRD analysis •  Design Reviews, Audits

•  Systems Architecture, DODAF and UML modeling •  Metric development and management,

•  Systems FMEA, Systems Analysis, Simula0on Modeling, Verifica0on

•  Technical Wri0ng •  Sta0s0cal Analysis

Aircra\ Systems

FAA/EASA requirements for component cer0fica0on, FAA Cer0fica0on Process, FAR Part 25, DO-‐160, D0-‐178x and D0-‐254/CMMI processes

Commercial –  Airbus A350, A380, A400 –  Boeing 747/757/767/777/787 –  Gulfstream, Bombardier

DOD –  B1, B2, F4, F15, F16, F22, C130, C17 –  Helicopters: Apache (AH64), Comanche, CH47, V-‐22

GE, Rolls Royce Engines; Gas and Air Turbines –  T45, T53, T55, ALF502 /507, L159, LTS101, AGT1500, T800, TF40 –  LF502/507, TFE731, CFE738, F124, F125, TFE1042 and TPE331

Special0es: –  Airborne Radar Systems, Diff. GPS landing systems, HUD, Control Systems, Thrust Reversers,

System and Component Tes0ng/Test Equipment, Pneuma0cs, engine bleed air over-‐heat detec0on system (OHDS), Satellite Telephone System Integra0on

Mul0ple Patents (9)

Space Systems

•  Extensive background on MILCOM Systems, Iridium, MUOS, and others

•  Communica0ons, Bus Systems, Mission Analyses, Ground Control, ORS, Constella0ons

•  ISR Systems •  Reac0on Control Subsystem •  AOCS

•  GPS, IMU, EO sensors, Simula0ons •  Electrical Power Subsystem •  Telemetry and Command Subsystem

•  RS232, RS422, RSS485, DOD 1553

Hardware Design

Electrical –  Circuit Design: analog, digital, RF and mixed signal circuit design –  Signal Integrity –  Power regula0on on-‐card design –  Configurable logic systems –  Parts and Components determina0on –  Standards: IPC–2222; IPC–2223; SM–782; Mil-‐P-‐55110 –  PCB design/layout/fab, Assembly Drawings (All toolsets) –  FMEA

Mechanical –  Design, fab, assembly of commercial, military and space hardware –  Proper0es of Materials –  3D solid modeling ; 2D and 3D mechanical analysis (Ansys-‐11.0) ; 3D fluid flow analysis

(Ansys/CFX-‐11.0) –  Electro/Mechanical packaging, rack and panel configura0ons, cabling and rou0ng,

configura0on control/ECO’s –  CAD/manual design/dra\ing, 2D/3D modeling, detailed mechanical assemblies

RECON Engineering

RECON Engineering Services Obsolescence/Legacy Engineering

•  Update older systems that rely on obsolete parts, discon0nued so\ware, and/or outdated processors wriben in older programming languages

•  Conduct current System Analysis and replacement development •  Concurrent Process Flow •  Deliverables include updated/validated PCB Database, Gerber files, drawings, test documenta0on, func0onally tested PCB’s, and Embedded So\ware programs

Electrical Hardware Reverse Engineering

Toolsets

Systems Engineering –  DOORS, Ra0onal Tool Set (ReqPro) –  Clearcase and Clearquest –  Matlab/Simulink/Mathema0ca

Embedded Systems –  Xilinx, Virtex, Cadence ModelSim

Electrical Design –  Mentor Expedi0on, Board Sta0on, Auto RE, DX Designer, Design Capture, Design Architect, Pantheon Intercept, Mosaic, Cadence Allegro, OrCAD, Valor, Gerb Tool, Hyperlinks, PSPICE

Mechanical Design –  Pro / Engineer, Siemens NX 7.x, SDRC Ideas, Solid Works, AutoCAD


Integrity alleviates program value risk

•  Greater design cycle visibility

•  Expanded customer interface throughout

•  Highly customized exper0se

•  Senior level oversight

•  Company-‐wide amtude of ownership

Art Bejarano Jr.

Case Study

Program: Orion Crew Vehicle Program Client: Honeywell

Scope: •  Program management •  Subcontract services •  Mechanical design and documenta0on •  Electrical circuit and PCB design •  Parts procurement •  Manufacturing and assembly

Outcomes:

•  Reduced turn 0me by over 40% •  Comple0on of five (5) test fixtures within 5 ½ months

Case Study

Program: Nepires Missile Program Client: Raytheon Missile Systems

Scope:

•  PCB design

•  Interfaced with mul0ple manufacturing vendors to meet customer requirements

•  Applied latest design and manufacturing capabili0es beyond the customer’s internal requirements

•  Manufacturing and assembly

Outcomes:

•  Reduced turn 0me by over 70%

•  Completed within budgetary targets

•  Successful first launch

Case Study

Orion Space System •  Working with Honeywell Space, designed, built, and tested 5 different System Test Equipment (STE’s) units

•  Different card types for the Orion Space Crew Explora0on Vehicle’s (CEV) Power and Data Unit (PDU) included: •  Pyro Events Controller (PEC) •  Network Switch Card (NSC) •  PDU Controller •  Solenoid Driver Output (SDO) •  Analog Digital Input/Output (ADIO) units

•  All STE’s delivered to Honeywell, Clearwater site

Case Study

Orion Space Program (cont.) INTEGRITY’s responsibili0es

•  Overall project management of STE development •  Interfaced directly with both Honeywell Management and Engineering, Tandel Systems Integra0on personnel, plus all subcontractors, contract shops and key suppliers and vendors

•  Requirements and Specifica0on Development •  Architecture comple0on •  STE design, review and verifica0on •  HW design and review •  CDR prep, presenta0on and customer buyoff •  Parts iden0fica0on, selec0on, buy and review •  Mechanical drawing genera0on from architecture to component level

•  PCB design, layout, fabrica0on & assembly

Case Study

Commercial AircraA •  Standards

•  EUROCAE ED-‐14D/RTCA DO-‐160D (Environmental and EMI/HIRF Hardware Test Standards), EUROCAE ED-‐12B/RTCA DO-‐178B (So\ware Test Standards) and RTCA DO-‐254 (Design Assurance Standards for Airborne Electronic Hardware)

•  A350 Extended Mechanical System Perimeter (EMSP) •  Validated over 30 ABD documents through mul0ple revisions •  Populated the DOORS database with flow down requirements that are linked from

the ABD0100 and ABD0200 requirements •  Established and con0nue to maintain trace links from the DOORS requirements to

lower level Honeywell systems •  Management of the EMSP System Development Plan and the EMSP Valida0on and

Verifica0on Plan •  Detailed tracking of Work Package documenta0on and hardware •  Evalua0ng and verifying the interconnec0vity between all Work Packages •  Audit support across all levels of program work assignments •  Test stand integra0on, checkout and commissioning •  Developing detailed component and systems integra0on procedures to authorize

ini0al ‘Power-‐On’ tes0ng

Case Study

Commercial AircraA (cont.) •  A380 Electrical Thrust Reverser Actua0on System (ETRAS)

•  Supported Preliminary and Cri0cal Design Reviews including Qualifica0on and Cer0fica0on Review mee0ngs.

•  Provided development, audit and release support for Valida0on and Verifica0on documenta0on deliverables.

•  Performed field tes0ng at General Electric in Ohio and at Prab & Whitney in Florida

•  Performed lab systems tes0ng for design assurance (all so\ware versions) and for mul0ple qualifica0on tests (so\ware versions for Airworthiness Authority approval)

•  Developed requirements based test procedures, performed the qualifica0on test and wrote the test reports that cover so\ware versions FCS2, FCS2+, FCS2++,

•  Updated Test Procedures for future so\ware revisions (FCS3)

Case Study

•  Interna9onal Space Sta9on Docking System –  Prime Contractor Boeing

•  INTEGRITY supported Honeywell tes0ng and analysis associated with linear/rotary actuators for the Low Impact Docking System (LIDS)

•  INTEGRITY supported Honeywell technical inves0ga0ons, design evalua0ons, and key supplier development issues using 6 Sigma/Lean process tools –  Presented analysis and recommenda0ons to Boeing customer during program

reviews

integrity engineering-2

Documents