Space systems. Small-auxiliary-spacecraft (SASC) to-launch-vehicle interface control document Ingestion-build-256245 apparatus and procedure for determining

apparatus and procedure for determining the distribution of tensile strength and tensile strain to failure of ceramic filaments in multifilament tows at ambient temperature

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ships or offshore structures to enable emergency evacuation as well as improved firefighting

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Space systems. Small-auxiliary-spacecraft (SASC) to-launch-vehicle interface control document Ingestion-build-256245 apparatus and procedure for determining1 Scope This International Standard provides small auxiliary spacecraft (SASC) and launch vehicle (LV) organizations with basic rules for writing an interface control document (ICD), and a general format for the document's presentation, when the SASC has an interface (I F) only with the LV. It is applicable to the necessary ICD items and restrictions peculiar to SASCs, these spacecraft being as defined in the contract between the launch agency and the