Space engineering - Fracture control
This ECSS Engineering Standard specifies the fracture control requirements to
be imposed on space segments of space systems and their related GSE.
The fracture control programme is applicable for space systems and related
GSE when required by ECSS-Q-ST-40 or by the NASA document NST 1700.7,
incl. ISS addendum.
The requirements contained in this Standard, when implemented, also satisfy
the fracture control requirements applicable to the NASA STS and ISS as
specified in the NASA document NSTS 1700.7 (incl. the ISS Addendum).
The NASA nomenclature differs in some cases from that used by ECSS. When
STS/ISS-specific requirements and nomenclature are included, they are
identified as such.
This standard may be tailored for the specific characteristic and constrains of a
space project in conformance with ECSS-S-ST-00.
ΚΩΔΙΚΟΣ ΠΡΟΪΟΝΤΟΣ:
CYS EN 16603-32-01:2014
This ECSS Engineering Standard specifies the fracture control requirements to
be imposed on space segments of space systems and their related GSE.
The fracture control programme is applicable for space systems and related
GSE when required by ECSS-Q-ST-40 or by the NASA document NST 1700.7,
incl. ISS addendum.
The requirements contained in this Standard, when implemented, also satisfy
the fracture control requirements applicable to the NASA STS and ISS as
specified in the NASA document NSTS 1700.7 (incl. the ISS Addendum).
The NASA nomenclature differs in some cases from that used by ECSS. When
STS/ISS-specific requirements and nomenclature are included, they are
identified as such.
This standard may be tailored for the specific characteristic and constrains of a
space project in conformance with ECSS-S-ST-00.