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10.8 Impact of Stealth Design
10.8.1 Lockheed F-117A Nighthawk
10.8.2 Northrop B-2 Spirit
10.8.3 Joint Strike Fighter – F-35 Lightning II
10.9 Technology Developments/Demonstrators
10.9.1 Fault Tolerant 270VDC Electrical Power
Generation System
10.9.2 Thermal and Energy Management Module
10.9.3 AFTI F-16 Flight Demonstration
11 System Design and Development
11.1 Introduction
11.1.1 Systems Design
11.1.2 Development Processes
11.2 System Design
11.2.1 Key Agencies and Documentation
11.2.2 Design Guidelines and Certification Techniques
11.2.3 Key Elements of the Development Process
11.3 Major Safety Processes
11.3.1 Functional Hazard Analysis (FHA)
11.3.2 Preliminary System Safety Analysis (PSSA)
11.3.3 System Safety Analysis (SSA)
11.3.4 Common Cause Analysis (CCA)
11.4 Requirements Capture
11.4.1 Top-Down Approach
11.4.2 Bottom-Up Approach
11.4.3 Requirements Capture Example
11.5 Fault Tree Analysis (FTA)
11.6 Dependency Diagram
11.7 Failure Modes and Effects Analysis (FMEA)
11.8 Component Reliability
11.8.1 Analytical Methods
11.8.2 In-Service Data
11.9 Dispatch Reliability
11.10 Markov Analysis
11.11 Development Processes
11.11.1 The Product Life Cycle
11.11.2 Concept Phase
11.11.3 Definition Phase
11.11.4 Design Phase
11.11.5 Build Phase
11.11.6 Test Phase (Qualification Phase)
11.11.7 Operate Phase
11.11.8 Disposal or Refurbish
11.11.9 Development Programme
11.11.10 ‘V' Diagram
11.12 Extended Operations (ETOPS)
12 Avionics Technology
12.1 Introduction
12.2 The Nature of Microelectronic Devices
12.2.1 Processors
12.2.2 Memory Devices
12.2.3 Digital Data Buses
12.2.4 A 429 Data Bus
12.2.5 MIL-STD-1553B
12.2.6 ARINC 629 Data Bus
12.2.7 COTS Data Buses
12.3 Data Bus Integration of Aircraft Systems
12.3.1 Experimental Aircraft Programme (EAP)
12.3.2 Airbus A330/340
12.3.3 Boeing 777
12.3.4 Regional Aircraft/Business Jets
12.3.5 A380 Avionics Architecture
12.3.6 Boeing 787 Avionics Architecture
12.3.7 COTS Data Buses – IEEE 1394
12.4 Fibre Optic Buses
12.5 Avionics Packaging Standards
12.5.1 Air Transport Radio (ATR)
12.5.2 Modular Concept Unit (MCU)
12.6 Typical LRU Architecture
12.7 Integrated Modular Avionics
13 Environmental Conditions
13.1 Introduction
13.2 Environmental Factors
13.2.1 Altitude
13.2.2 Temperature
13.2.3 Contamination by Fluids
13.2.4 Solar Radiation
13.2.5 Rain, Humidity, Moisture
13.2.6 Fungus
13.2.7 Salt Fog/Salt Mist
13.2.8 Sand and Dust
13.2.9 Explosive Atmosphere
13.2.10 Acceleration
13.2.11 Immersion
13.2.12 Vibration
13.2.13 Acoustic Noise
13.2.14 Shock
13.2.15 Pyroshock
13.2.16 Acidic Atmosphere
13.2.17 Temperature, Humidity, Vibration, Altitude
13.2.18 Icing/Freezing Rain
13.2.19 Vibro-Acoustic, Temperature
13.2.20 RF Radiation
13.2.21 Lightning
13.2.22 Nuclear, Biological and Chemical
13.3 Testing and Validation Process
Index
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