BS ISO 15864:2004

Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
  3.1 Terms and definitions
  3.2 Abbreviated terms
4 General requirements
  4.1 Testing philosophy
  4.2 Tailoring of requirements
  4.3 Development tests
  4.4 Qualification tests
  4.5 Acceptance tests
  4.6 Proto-flight tests
  4.7 Prelaunch validation tests
  4.8 Retest
  4.9 Test documentation
  4.10 Tests facilities and other requirements
5 Spacecraft system tests
  5.1 Test items and sequence
  5.2 Test levels and duration
6 Subsystem/unit tests
  6.1 Test items and sequence
  6.2 Test levels and duration
7 Test requirements
  7.1 General
  7.2 Functional test
  7.3 Electromagnetic compatibility (EMC) test
  7.4 Magnetic field test
  7.5 Antenna pattern test
  7.6 Optical alignment measurement
  7.7 Physical property measurement
  7.8 Dynamic balance
  7.9 Launcher/spacecraft interface test
  7.10 Static load test
  7.11 Acceleration test
  7.12 Modal survey
  7.13 Sinusoidal vibration test
  7.14 Random vibration test
  7.15 Acoustic test
  7.16 Shock test
  7.17 Thermal balance test
  7.18 Thermal vacuum test
  7.19 Thermal cycle test
  7.20 Pressure test
  7.21 Leakage test
  7.22 Burn-in and wear-in test
  7.23 Tracking and control system/spacecraft compatibility test

Provides the baseline standard on the subject of testing at the system, subsystem and unit levels for applicable unmanned spacecraft programmes. It also provides the requirements for documentation associated with testing activities.