This site describes design and test practices that contributed to the success of NASA spaceflight missions up to year 1999. This document, "NASA Reliability Preferred Practices for Design and Test," was prepared by the NASA Reliability and Maintainability Steering Committee in February 1999. Each practice was vetted by participating NASA Centers as a valid “NASA-wide” practice. In 1998, NASA received the IEEE Reliability Society's first Company of the Year award in recognition of the publication of this document and the "Recommended Techniques for Effective Maintainability." Please note that these “preferred practices” have not been reviewed for consistency with current engineering practices. For possible updates and preferred practices (lessons learned) after 1998, use the NASA Lessons Learned Information System.
Tech Memo 4322A, Feb 1999
This section contains reliability design practices provided for use throughout NASA and the aerospace community to assist in the design and development of highly reliable equipment and assemblies. The practices include recommended analysis procedures, redundancy considerations, parts selection, environmental requirements considerations, and test requirements and procedures. Each practice document defines the practice and discusses its benefits, spacecraft applications, implementation method, technical rationale, and impact of non-performance, and it also lists references and related practices.
Environmental Series
- Practice No. PD-EC-1101 - Environmental Factors [LL]
- Practice No. PD-EC-1102 - Meteoroids/Space Debris
- Practice No. PD-EC-1103 - Nickel-Cadmium Conventional Spacecraft Battery Handling and Storage Practice
- Practice No. PD-EC-1104 - Monitoring Spacecraft Exposure to Magnetic Fields
- Practice No. PD-EC-1105 - Solar Flare Proton & Heavy Ion Modeling for Single Event Effects
- Practice No. PD-EC-1106 - Plasma Noise in EMI Design
- Practice No. PD-EC-1107 - Micrometeorite Protection
- Practice No. PD-EC-1108 - Super Ni-Cd Spacecraft Battery Handling and Storage Practice
- Practice No. PD-EC-1109 - Ni-H2 Spacecraft Battery Handling and Storage Practice
- Practice No. PD-EC-1110 - Optical Fiber Cable Terminations and Procedures
Engineering Design Series
- Practice No. PD-ED-1201 - EEE Parts Derating
- Practice No. PD-ED-1202 - High Voltage Power Supply Design and Manufacturing Practices
- Practice No. PD-ED-1203 - Class S Parts in High Reliability Applications
- Practice No. PD-ED-1204 - Part Junction Temperature
- Practice No. PD-ED-1205 - Welding Practices for 2219 Aluminum and Inconel
- Practice No. PD-ED-1206 - Power Line Filters
- Practice No. PD-ED-1207 - Magnetic Design Control for Science Instruments
- Practice No. PD-ED-1208 - Static Cryogenic Seals for Launch Vehicle
- Practice No. PD-ED-1209 - Ammonia-Charged Aluminum Heat Pipes with Extruded Wicks
- Practice No. PD-ED-1210 - Assessment and Control of Electrical Charges
- Practice No. PD-ED-1211 - Combination Methods for Deriving Structural Design Loads
- Practice No. PD-ED-1212 - Design & Analysis of Circuits for Worst Case Environments and Part Variations
- Practice No. PD-ED-1213 - Electrical Shielding of Power, Signal, and Control Cables
- Practice No. PD-ED-1214 - Electrical Grounding Practices for Aerospace Hardware
- Practice No. PD-ED-1215.1 - Preliminary Design Review
- Practice No. PD-ED-1215.2 - Hardware Review / Certification Requirement
- Practice No. PD-ED-1215-3 - Critical Design Review for Unmanned Missions
- Practice No. PD-ED-1215-4 - Common Review Methods
- Practice No. PD-ED-1215-5 - Pre-Ship Review
- Practice No. PD-ED-1215.6 - Mission Readiness Review
- Practice No. PD-ED-1216 - Active Redundancy
- Practice No. PD-ED-1217 - Structural Laminate Composites for Space Applications
- Practice No. PD-ED-1218 - Application of Ablative Composites to Nozzles for Reusable Solid Rocket Motors
- Practice No. PD-ED-1219 - Vehicle Integration/Tolerance Build-up Practices
- Practice No. PD-ED-1220 - Demagnetization of Ferromagnetic Parts
- Practice No. PD-ED-1221 - Battery Selection Practice for Aerospace Power Systems
- Practice No. PD-ED-1222 - Magnetic Field Restraints for Spacecraft Systems and Subsystems
- Practice No. PD-ED-1223 - Vacuum Seals Design Criteria
- Practice No. PD-ED-1224 - Design Considerations for Fluid Tubing Systems
- Practice No. PD-ED-1225 - Conducted and Radiated Emissions Design Requirements
- Practice No. PD-ED-1226 - Thermal Design Practices for Electronic Assemblies
- Practice No. PD-ED-1227 - Controlling Stress Corrosion Cracking in Aerospace Applications
- Practice No. PD-ED-1228 - Independent Verification and Validation of Embedded Software
- Practice No. PD-ED-1229 - Selection of Electric Motors for Aerospace Applications
- Practice No. PD-ED-1230 - System Design Analysis Applied to Launch Vehicle Configurations
- Practice No. PD-ED-1231 - Design Considerations for Lightning Strike Survivability
- Practice No. PD-ED-1232 - Spacecraft Orbital Anomaly Report (SOAR) Systems
- Practice No. PD-ED-1233 - Contamination Control Program
- Practice No. PD-ED-1234 - Global Positioning System (GPS) Timing System
- Practice No. PD-ED-1235 - Over-Speed Protection System for DC Motor Driven Cranes
- Practice No. PD-ED-1236 - EEE Parts Selection Criteria for Flight Systems
- Practice No. PD-ED-1238 - Spacecraft Electrical Harness Design Practice
- Practice No. PD-ED-1239 - Spacecraft Thermal Control Coatings Design and Application
- Practice No. PD-ED-1240 - Identification, Control, and Management of Critical Items Lists
- Practice No. PD-ED-1241 - Contamination Budgeting for Space Optical Systems
- Practice No. PD-ED-1242 - Design Considerations for Space Trusses
- Practice No. PD-ED-1243 - Fault Protection
- Practice No. PD-ED-1244 - Design Practice to Control Interference from Electrostatic Discharge (ESD)
- Practice No. PD-ED-1245 - Magnetic Dipole Allocation
- Practice No. PD-ED-1246 - Fault Tolerant Design
- Practice No. PD-ED-1247 - Spacecraft Lessons Learned Reporting System
- Practice No. PD-ED-1248 - Spacecraft Data Systems (SDS) Hardware Design Practice
- Practice No. PD-ED-1249 - Electrostatic Discharge (ESD) Control in Flight Hardware
- Practice No. PD-ED-1250 - Pre-Flight Problem/Failure Reporting Procedures
- Practice No. PD-ED-1251 - Instrumentation System Design and Installation for Launch Vehicles
- Practice No. PD-ED-1252 - Material Selection Practices
- Practice No. PD-ED-1253 - Arcjet Thruster Design Considerations for Satellites
- Practice No. PD-ED-1254 - Design Reliable Ceramic Components with CARES Code
- Practice No. PD-ED-1255 - Problem Reporting and Corrective Action System
- Practice No. PD-ED-1256 - Automatic Transfer Switches (ATS) in Critical Applications
- Practice No. PD-ED-1257 - Solid Rocket Motor Joint Reliability
- Practice No. PD-ED-1258 - Space Radiation Effects on Electronic Components in Low-Earth Orbit
- Practice No. PD-ED-1259 - Acoustic Noise Requirements
- Practice No. PD-ED-1260 - Radiation Design Margin Requirement
- Practice No. PD-ED-1261 - Characterization of RF Subsystem Susceptibility to Spurious Signals
- Practice No. PD-ED-1262 - Subsystem Inheritance Review
- Practice No. PD-ED-1263 - Contamination Control of Space Optical Systems
- Practice No. PD-ED-1264 - Integrated Optical Performance Modeling of X-Ray Systems
- Practice No. PD-ED-1265 - Precision Diamond Turning of Aerospace Optical Systems
- Practice No. PD-ED-1266 - Binary and Hybrid Optics for Space Applications
- Practice No. PD-ED-1267 - Check Valve Reliability in Aerospace Applications
- Practice No. PD-ED-1268 - High Performance Liquid Hydrogen Turbopumps
- Practice No. PD-ED-1269 - High Performance Liquid Oxygen Turbopumps
- Practice No. PD-ED-1272 - Manned Space Vehicle Battery Safety
- Practice No. PD-ED-1273 - Quantitative Reliability Requirements Used as Performance-Based Requirements for Space Systems.
Analysis Series
- Practice No. PD-AP-1301 - Surface Charging / ESD Analysis
- Practice No. PD-AP-1302 - Independent Review of Reliability Analyses
- Practice No. PD-AP-1303 - Part Electrical Stress Analyses
- Practice No. PD-AP-1304 - Problem/Failure Report Independent Review and Approval
- Practice No. PD-AP-1305 - Risk Rating of Problem/Failure Reports
- Practice No. PD-AP-1306 - Thermal Analysis of Electronic Assemblies to the Piece Part Level
- Practice No. PD-AP-1307 - Failure Modes, Effects And Criticality Analysis (FMECA)
- Practice No. PD-AP-1308 - Electromagnetic Interference Analysis of Circuit Transients
- Practice No. PD-AP-1309 - Analysis of Radiated EMI From ESD Events Caused by Space Charging
- Practice No. PD-AP-1310 - Spurious Radiated Interference Awareness
- Practice No. PD-AP-1311 - Computational Fluid Dynamics (CFD) in Launch Vehicle Applications
- Practice No. PD-AP-1312 - The Team Approach to Fault-Tree Analysis
- Practice No. PD-AP-1313 - System Reliability Assessment Using Block Diagraming Methods
- Practice No. PD-AP-1314 - Sneak Circuit Analysis Guideline for Electromechanical Systems
- Practice No. PD-AP-1315 - Redundancy Switching Analysis
- Practice No. PD-AP-1316 - Thick Dielectric Charging/Internal Electrostatic Discharge (IESD)
- Practice No. PD-AP-1317 - Flight Load Analysis as a Spacecraft Design Tool
- Practice No. PD-AP-1318 - Structural Stress Analysis
- Practice No. PD-AP-1319 - Redundancy Verification Analysis
Test Series
- Practice No. PT-TE-1401 - EEE Parts Screening
- Practice No. PT-TE-1402 - Thermal Cycling
- Practice No. PT-TE-1403 - Thermographic Mapping of PC Boards
- Practice No. PT-TE-1404 - Thermal Test Levels & Durations
- Practice No. PT-TE-1405 - Powered-On Vibration
- Practice No. PT-TE-1406 - Sinusoidal Vibration
- Practice No. PT-TE-1407 - Assembly Acoustic Tests
- Practice No. PT-TE-1408A - Pyrotechnic Shock Testing (revised to reflect "powered" test mode)
- Practice No. PT-TE-1409 - Thermal-Vacuum Versus Thermal-Atmospheric Tests of Electronic Assemblies
- Practice No. PT-TE-1410 - Selection of Spacecraft Materials and Supporting Vacuum Outgassing Data
- Practice No. PT-TE-1411 - Heat Sinks for Parts Operated in Vacuum
- Practice No. PT-TE-1412 - Environmental Test Sequencing
- Practice No. PT-TE-1413 - Random Vibration Testing
- Practice No. PT-TE-1414 - Electrostatic Discharge (ESD) Test Practices
- Practice No. PT-TE-1415 - Power System Corona Testing
- Practice No. PT-TE-1416 - Radiated Susceptibility System Verification
- Practice No. PT-TE-1417 - Electrical Isolation Verification (DC)
- Practice No. PT-TE-1418 - Qualification of Non-Standard EEE Parts in Spaceflight Applications
- Practice No. PT-TE-1419 - Vibroacoustic Qualification Testing of Payloads, Subsystems, and Components
- Practice No. PT-TE-1420 - Sine-Burst Load Test
- Practice No. PT-TE-1421 - Eddy Current Testing of Aerospace Materials
- Practice No. PT-TE-1422 - Ultrasonic Testing of Aerospace Materials
- Practice No. PT-TE-1423 - Radiographic Testing of Aerospace Materials
- Practice No. PT-TE-1424 - Leak Testing of Liquid Hydrogen and Liquid Oxygen Propellant Systems
- Practice No. PT-TE-1425 - Magnetic Particle Testing of Aerospace Materials
- Practice No. PT-TE-1426 - Penetrant Testing of Aerospace Materials
- Practice No. PT-TE-1427 - Rocket Engine Technology Test Bed Practice
- Practice No. PT-TE-1428 - Practice of Reporting Parts, Materials, and Safety Problems (Alerts)
- Practice No. PT-TE-1429 - Integration and Test Practices to Eliminate Stresses on Electrical and Mechanical Components
- Practice No. PT-TE-1430 - Short Circuit Testing for Nickel/Hydrogen Battery Cells
- Practice No. PT-TE-1431 - Voltage/Temperature Margin Testing
- Practice No. PT-TE-1432 - RF Breakdown Characterization
- Practice No. PT-TE-1433 - Mechanical Fastener Inspection System
- Practice No. PT-TE-1434 - Battery Verification through Long-Term Simulation
- Practice No. PT-TE-1435 - Verification of RF Hardware Design Performance
- Practice No. PT-TE-1436 - Advanced Computed X-Ray Tomography
- Practice No. PT-TE-1437 - End to End Compatibility and Mission Simulation Testing
- Practice No. PT-TE-1438 - Reliability Considerations for Launch Vehicle Command Destruct Systems
- Practice No. PT-TE-1439 - Systems Test Considerations for High Performance Liquid Propellant Rocket Engines
- Practice No. PT-TE-1440 - Modal Testing: Measuring Dynamic Structural Characteristics
- Practice No. PT-TE-1441 - Design of an Improved Gas Transfer Valve for Leak Tight Testing
- Practice No. PT-TE-1442 - Design of a Small Apparatus for Improved Vibration/Thermal Testing
This section contains reliability design guidelines for consideration by the aerospace community. The guidelines presented in this section contain valuable information that, in the opinion of the sponsoring activity, represents a technically credible process that could be applied to ongoing NASA programs/projects. Unlike a reliability design practice, a guideline lacks specific operational experience or data to indicate that a topic area has contributed to mission success. However, a guideline does contain information that represents current “best thinking” on a particular topic and is a well thought out approach to resolving a particular issue or problem. The Reliability and Maintainability Steering Committee agreed unanimously with the appropriateness of the approach.
Engineering Design Series
- Guideline No. 2201 - Fastener Standardization and Selection Considerations
- Guideline No. 2202 - Design Considerations for Selection of Thick-Film Microelectronic Circuits
- Guideline No. 2203 - Design Checklists for Microcircuits
- Guideline No. 2204 - Concurrent Engineering Guideline for Aerospace Systems
- Guideline No. 2205 - Design and Manufacturing Guideline for Aerospace Composites
- Guideline No. 2206 - Selection of Compatible Materials for Use with Fluorine
- Guideline No. 2207 - Designing for Dormant Reliability
- Guideline No. 2208 - Fabrication of Gaseous and Liquid Fluorine Systems
- Guideline No. 2209 - Spacecraft Deployed Appendage Design Guidelines
- Guideline No. 2210 - Fiber-Reinforced Polymer Composite Material Selection
- Guideline No. 2211 - Coordinate Systems for Attitude Determination and Control
- Guideline No. 2213 - Management of Limited Failure Analysis Resources for EEE Parts
- Guideline No. 2214 - Marman Clamp System Design Guidelines
Analytical Procedures Series
- Guideline No. 2301 - Earth Orbit Environmental Heating
- Guideline No. 2302 - Thermal Analysis of Spacecraft Hardware Guideline
- Guideline No. 2303 - Spectral Fatigue Reliability
- Guideline No. 2304 - Fracture Mechanics Reliability
- Guideline No. 2305 - Structural Analysis in the Design of Optical Mirrors
Test Element Series
- Guideline No. 2401 - EMC Guideline for Payloads, Subsystems, and Components
- Guideline No. 2402 - Near Field Measurement for Large Aperture Antenna Pattern Determination
- Guideline No. 2403 - Spacecraft Deployed Appendage Test Guidelines
- Guideline No. 2404 - Guideline for Use of Fizeau Interferometer in Optical Testing
This section contains design and procedural practices that have contributed to successful ground support of spaceflight and ground-based aerospace programs. The information presented in this section is for use throughout NASA and the aerospace community to assist in the design, development, and operation of highly reliable ground support equipment and assemblies. This material is primarily concerned with design and test techniques, procedures for control of critical items, and control of environmental influences on successful launch.
- Practice No. 3001 - Flow Fuses for Elimination of Hazards in Pneumatic and Hydraulic Systems
- Practice No. 3002 - Fail Safe Firex/Deluge System
- Practice No. 3003 - Redundancy in Critical Mechanical Systems
- Practice No. 3004 - Use of Design Review Checklists for Space Shuttle GSE
- Practice No. 3005 - Identification, Control, and Management of GSE Critical Items
- Practice No. 3006 - Environmental Test Methods for Ground Support Equipment
- Practice No. 3007 - Redundancy Considerations for Ground Communication Systems
- Practice No. 3008 - Electrostatic Discharge Control for GSE
- Practice No. 3009 - Uninterruptable Power Supply Systems (UPS)
- Practice No. 3010 - Oil-Free Vacuum Pump in the LOX/LH2 Transfer System
- Practice No. 3011 - Foreign Object Debris (FOD) Programs at KSC
Program Management Series
A fundamental key to program and mission success is the development of systems that are reliable and affordable to operate and maintain with today's limited resources. Early definition of both hardware and software requirements that provide the capability for rapid restoration when failures occur is essential. While incorporation of a maintainability program may require some additional early investment, the resulting benefits will include operational cost savings and improved system availability. The techniques included in this section are intended to provide management personnel with an understanding of all information necessary to develop, foster, and integrate a successful maintainability program that will enhance mission success and lower overall costs. Each technique provides high-level information on a specific subject, and can be tailored or expanded to achieve optimum application.
- Technique No. PM-1 - Benefits of Implementing Maintainability on NASA Programs
- Technique No. PM-2 - Maintainability Program Management Considerations
- Technique No. PM-3 - Maintenance Concept for Space Systems
- Technique No. PM-4 - Preventive Maintenance Strategies Using Reliability Centered Maintenance
Design Factors and Engineering Series
- Technique No. DFE-1 - Selection of Robotically Compatible Fasteners and Handling Mechanisms
- Technique No. DFE-2 - False Alarm Mitigation Techniques
- Technique No. DFE-3 - Common Charge Points for Lubrication Systems for Mechanical Ground Support Equipment
- Technique No. DFE-4 - Use of Digital Potentiometers in Electrically Powered Systems
- Technique No. DFE-5 - Ground Piping SystemsColor Coding and Identification
- Technique No. DFE-6 - Software Design for Maintainability
- Technique No. DFE-7 - Fault Detection, FaultIsolation and Recovery (FDIR) Techniques
Analysis and Test Series
The objective of the Maintainability function is to influence system design such that the end product can be maintained in a cost effective operational condition with minimum downtime. In order for the Maintainability discipline to provide maximum influence to a program, design principles to obtain these objectives must be implemented early in the design phase. Techniques that have proven to be beneficial on previous programs are presented in this section as design recommendations for future programs.
- Technique No. AT-1 - Neutral Buoyancy Simulation of On-Orbit Maintenance
- Technique No. AT-2 - Mean-Time-To-Repair Predictions
- Technique No. AT-3 - Availability Prediction and Analysis
- Technique No. AT-4 - Availability, Cost, and Resource Allocation (ACARA) Model to Support Maintenance Requirements
- Technique No. AT-5 - Rocket Engine Failure Prediction Using an Average Signal Power Technique
- Technique No. AT-6 - Wear Particle Analysis Using Ferrography
- Technique No. AT-7 - Maintenance & Test Criteria for Circuit Breakers
- Technique No. AT-8 - Vibration Analysis of Rotating Ground Support Machinery
- Technique No. AT-9 - Thermography
- Technique No. AT-10 - Ultrasound Testing
Operations and Operational Design Techniques
This section provides a rich source of ideas to any organization that is involved in either spaceflight operations or design to support those operations. The techniques reflect actual spaceflight operations experience and related field experience that can be used to achieve continuous improvement. They can provide a mechanism for feedback from operators of flight hardware to system designers to make the systems easier, safer, and less costly to operate. Also, they provide the design engineer with valuable information on the latest technology advances in the operations environment. These techniques also can serve as a communications tool for operations personnel, allowing for transfer of knowledge and enhancement of professional development. The techniques contained herein are the most up-to-date NASA operational processes, process improvements, and feedback to design engineers, all of which are dedicated to making NASA systems as maintainable and cost efficient as possible.
- Technique No. OPS-1 - SRB Refurbishment Practices
- Technique No. OPS-2 - Electrical Connector Protection
- Technique No. OPS-3 - Robotic Removal and Application ofSRB Thermal Systems
- Technique No. OPS-4 - GHe Purging of H2 Systems
- Technique No. OPS-5 - Programmable Logic Controller
- Technique No. OPS-6 - DC Drive - Solid State Control
- Technique No. OPS-7 - AC - Variable Frequency DriveSystems
- Technique No. OPS-8 - Fiber Optic Systems
- Technique No. OPS-9 - Pneumatic Systems -Pilot-Controlled Loaded Pressure RegulatorLoading
- Technique No. OPS-10 - Modular Automatic Power SourceSwitching Device
- Technique No. OPS-11 - Pneumatic System ContaminationProtection
- Technique No. OPS-12 - Fault Isolation Using TerminalBlocks
- Technique No. OPS-13 - Predictive Maintenance Program
- Technique No. OPS-14 - Computer-Aided Laser ShaftAlignment of Rotating Machinery
- Technique No. OPS-15 - Facility Chilled Water for ThermalConditioning Unit
- Technique No. OPS-16 - Use of GN2 for ValveCorrosion Control
- Technique No. OPS-17 - Electrical Equipment Protectionfrom Liquid Intrusion
- Technique No. OPS-18 - Orbiter S-Band Uplink MonitoringSystem
- Technique No. OPS-19 - Maintainability Considerations inEVA Design: An Astronaut's Perspective