SS-EN-16603-20-01 Space engineering - Multipactor, design and test

SS-EN-16603-20-01 - 2020 EDITION - CURRENT


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This standard defines the requirements and recommendations for the design and test of RF components and equipment to achieve acceptable performance with respect to multipactor-free operation in service in space. The standard includes: - verification planning requirements, - definition of a route to conform to the requirements, - design and test margin requirements, - design and test requirements, and - informative annexes that provide guidelines on the design and test processes. This standard is intended to result in the effective design and verification of the multipactor performance of the equipment and consequently in a high confidence in achieving successful product operation. This standard covers multipactor events occurring in all classes of RF satellite components and equipment at all frequency bands of interest. Operation in single carrier CW and pulse modulated mode are included, as well as multi-carrier operations. A detailed clause on secondary emission yield is also included. This standard does not include breakdown processes caused by collisional processes, such as plasma formation. This standard is applicable to all space missions. This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.

To find similar documents by classification:

49.140 (Space systems and operations Including space data and information transfer systems, and ground support equipment for launch site operations)

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Designation Name

SS-EN 16603-20-01:2020

Revision Level

2020 EDITION

Status

Current

Publication Date

Sept. 30, 2020

Language(s)

English

Page Count

80

International Equivalent

EN 16603-20-01:2020(IDT)