NASA Office of Logic Design

A scientific study of the problems of digital engineering for space flight systems,
with a view to their practical solution.

Guide to the Use of this Monograph

Foreward

CONTENTS

1. INTRODUCTION

2. STATE OF THE ART

2.1 Spaceborne Computer Functions
2.2 System Design
2.3 Physical Characteristics
2.4 Environmental Design Factors
2.5 Reliability and Fault Tolerance
2.6 Testing and Checkout

3. DESIGN CRITERIA

3.1 Design Tradeoffs
3.2 System Design
3.3 Simulation
3.4 Testing and Checkout
3.5 Reliability and Fault Tolerance

4. RECOMMENDED PRACTICES

4.1 Design Tradeoffs
4.2 System Design
4.3 Simulation
4.4 Testing and Checkout
4.5 Reliability and Fault Tolerance

REFERENCES

GLOSSARY

NASA SPACE VEHICLE DESIGN CRITERIA MONOGRAPHS ISSUED TO DATE

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Last Revised: February 03, 2010
Digital Engineering Institute
Web Grunt: Richard Katz