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when the exhaust and cooling systems are ducted to a remote site their noise contribution is not to be included in this part of ISO 8528
The concept of the BRA
spectrometric measure metric of the calibration solutions
This part of the Technical Report provides a context model for the other parts of this Technical Report applying general architecture standards
Space systems. Prevention of break-up of unmanned spacecraft Ingestion-build-48024 when the exhaust and cooling1 Scope This International Standard defines the requirements to reduce the risk of in orbit break up of unmanned spacecraft, both during and after their operational lives. The aim would be met by reducing the possibility of a break up caused by an unplanned internally caused event and by depleting to a safe level all the sources of stored energy at the end of a spacecrafts life. This International Standard is designed for use in planning, verifying,
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