NASA STD 7002 : 0

PARAGRAPH
DOCUMENT HISTORY LOG
FOREWORD
1 SCOPE
  1.1 Scope
  1.2 Purpose
  1.3 Applicability
2 APPLICABLE DOCUMENTS
  2.1 General
  2.2 Government documents
      2.2.1 Standards
  2.3 Order of precedence
3 DEFINITIONS
  3.1 Protoflight hardware
  3.2 Prototype hardware
4 REQUIREMENTS
  4.1 Payload test requirements matrix (protoflight program)
  4.2 Mechanical tests
      4.2.1 Strength
      4.2.2 Sinusoidal sweep vibration (5 to 50 hertz [Hz])
            ELV and STS payloads
      4.2.3 Random vibration and acoustics
      4.2.4 Shock (mechanical and pyro)
      4.2.5 Modal survey
      4.2.6 Pressure profile
      4.2.7 Appendage deployment
  4.3 Thermal tests
      4.3.1 Thermal/vacuum and ambient pressure thermal
            cycling
      4.3.2 Thermal balance
      4.3.3 Bakeout
      4.3.4 Leak test for sealed components
  4.4 EMI tests
  4.5 Functional tests
      4.5.1 Electrical interface
      4.5.2 Comprehensive performance
      4.5.3 Failure-free performance
      4.5.4 End-to-end compatibility tests and mission
            simulations
      4.5.5 Life test program
      4.5.6 Mass properties verification
5 GUIDANCE
  5.1 Intended use
  5.2 Key word listing

Specifies selected environmental exposure tests for hardware operating in earth orbit. The tests included are generally regarded as the most critical and the ones having the highest cost and schedule impact. Also includes functional demonstration tests necessary to verify the capability of the hardware to perform its intended function (with and without environmental exposure as appropriate).