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DIN EN 16603-32-02

Space engineering - Structural design and verification of pressurized hardware; English version EN 16603-32-02:2014

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Organization: DIN
Publication Date: 1 October 2014
Status: active
Page Count: 85
ICS Code (Space systems and operations): 49.140
scope:

This Standard defines the structural design verification of metallic and nonmetallic pressurized hardware which includes pressure vessels, pressurized structures, pressure components (such as valves, pumps, lines, fittings, and hoses), and special pressurized equipment (e.g. batteries, heat pipes, cryostats, sealed containers, hazardous fluids container). External supports and structural interfaces of pressurized hardware are not covered by this standard. Solid propellant motor cases are not covered by this standard.

Objectives of the associated verification process are primarily to demonstrate the qualification of design and performance, as meeting all specified requirements, and to ensure that the flight hardware is free from workmanship defects and acceptable for flight.

This Standard applies to all space products and in particular to launch vehicles, transfer vehicles, re-entry vehicles, spacecraft, space station, landing probes and rovers, sounding rockets, payloads and instruments.

This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.

Document History

DIN EN 16603-32-02
October 1, 2014
Space engineering - Structural design and verification of pressurized hardware; English version EN 16603-32-02:2014
This Standard defines the structural design verification of metallic and nonmetallic pressurized hardware which includes pressure vessels, pressurized structures, pressure components (such as valves,...
November 1, 2013
Space engineering - Structural design and verification of pressurized hardware; English version FprEN 16603-32-02:2013
A description is not available for this item.

References

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