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for larger ignition sources
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Space systems. Format for spacecraft launch environment test report Ingestion-build-266356 for larger ignition sources1 Scope This International Standard provides a specific format to report the test process and results of spacecraft (SC) qualification to the launch environment. The following types of tests are considered: static load; modal survey; sine vibration; acoustic noise; random vibration; shock; and electromagnetic compatibility (EMC). The definition of test specifications and test requirements are derived from launch vehicle (LV) users manuals as defined