TS EN 16603-60-20 PDF | Request Standard

TS EN 16603-60-20

Space engineering - Star sensor terminology and performance specification

This Standard specifies star sensor performances as part of a space project. The Standard covers all aspects of performances, including nomenclature, definitions, and performance requirements for the performance specification of star sensors. The Standard focuses on: – performance specifications (including the impact of temperature, radiation and straylight environments); – robustness (ability to maintain functionalities under non nominal environmental conditions). Other specification types, for example mass and power, housekeeping data and data structures, are outside the scope of this Standard. This Standard also proposes a standard core of functional interfaces defined by unit suppliers and avionics primes in the context of Space AVionics Open Interface aRchitecture (SAVOIR) initiative. When viewed from the perspective of a specific project context, the requirements defined in this Standard should be tailored to match the genuine requirements of a particular profile and circumstances of a project. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.

Standard by TSE, 9.11.2020

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About This Item

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TS EN 16603-60-20 is a space engineering standard that addresses the terminology, definitions and performance specification framework for star sensors used in space projects. Star sensors are optical attitude sensors that determine spacecraft orientation from star imagery, so the subject of this standard is not only what the device is called, but also how its performance is defined and stated.

What the performance specification focuses on

The standard covers star sensor performance in a broad sense, with emphasis on nomenclature, definitions and performance requirements. In technical context, it gives particular attention to environmental influences such as temperature, radiation and stray light, because these can affect image quality, star identification and the stability of attitude determination. It also addresses robustness, meaning the ability to keep the sensor functional under non-nominal environmental conditions.

Boundaries of the document and interface context

Other specification types are explicitly outside the scope, including mass and power, housekeeping data and data structures. The standard also proposes a common core of functional interfaces defined by unit suppliers and avionics primes in the context of the SAVOIR initiative. In a project setting, the requirements are intended to be tailored to the genuine needs and constraints of a specific mission profile, making the document a common reference for describing star sensor performance rather than a one-size-fits-all system specification.

SKU: 0950cf78f915

  • Publication Date: 9.11.2020
  • Standard Status: U (Yürürlükteki Standard/Standard)
  • Publisher: TSE
  • Document Language: en
  • ICS Classification: 01.040.49 Uçak ve Uzay Taşıt Mühendisliği (Terimler); 49.140 Uzay Sistemleri ve Operasyonları
  • Pages: 91
  • Source Standard: EN 16603-60-20:2020
  • International Equivalents: EN 16603-60-20-EQV

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