GET https://dev.normadoc.fr/products/ieee-1101-7-1995-ieee00001657-240767

Components

3 Twig Components
5 Render Count
3 ms Render Time
74.0 MiB Memory Usage

Components

Name Metadata Render Count Render Time
ProductState
"App\Twig\Components\ProductState"
components/ProductState.html.twig
2 0.60ms
ProductMostRecent
"App\Twig\Components\ProductMostRecent"
components/ProductMostRecent.html.twig
2 1.68ms
ProductType
"App\Twig\Components\ProductType"
components/ProductType.html.twig
1 0.30ms

Render calls

ProductState App\Twig\Components\ProductState 66.0 MiB 0.39 ms
Input props
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          New IEEE Standard - Inactive-Withdrawn.<br />\n
          Withdrawn Standard. Withdrawn Date: Jan 15, 2001. The design requirements for a module designated for use in spacecraft, boosters, and other highly rugged, conductively cooled environments are established in this standard. The requirements herein serve to specify the mechanical design of the module. Dimensions and tolerances for racks, modules, printed wiring boards, backplanes, and other connector-related dimensions that are specific to the use of 300-pin and 396-pin connectors are given. These dimensions and tolerances are designed to ensure mechanical function and interoperability.<br />\n
          \t\t\t\t<br />\n
          This standard establishes the design requirements for a module designated for use in spacecraft, boosters, and other highly rugged, conductively cooled environments. The requirements herein serve to specify the mechanical design of the module.<br />\n
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Attributes
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Component
App\Twig\Components\ProductState {#93008
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          New IEEE Standard - Inactive-Withdrawn.<br />\n
          Withdrawn Standard. Withdrawn Date: Jan 15, 2001. The design requirements for a module designated for use in spacecraft, boosters, and other highly rugged, conductively cooled environments are established in this standard. The requirements herein serve to specify the mechanical design of the module. Dimensions and tolerances for racks, modules, printed wiring boards, backplanes, and other connector-related dimensions that are specific to the use of 300-pin and 396-pin connectors are given. These dimensions and tolerances are designed to ensure mechanical function and interoperability.<br />\n
          \t\t\t\t<br />\n
          This standard establishes the design requirements for a module designated for use in spacecraft, boosters, and other highly rugged, conductively cooled environments. The requirements herein serve to specify the mechanical design of the module.<br />\n
          The purpose of this standard is the specification of dimensions and tolerances that will ensure the mechanical intermatability of space and highly ruggedized modules within associated subracks. Modules aspect ratios and materials/processes of current standards do not cover needs. This lack has resulted in emergence of a defacto mechanical standard for space modules, currently being produced by multiple companies. The working group will define parameters to better accommodate high dynamic mechanical stresses, limited thermal dissipation, and use of space qualifiable materials and processes. The defacto space applications standard defined by the Advanced Spaceborne Computer Module will be encompassed.
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ProductType App\Twig\Components\ProductType 68.0 MiB 0.30 ms
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          Withdrawn Standard. Withdrawn Date: Jan 15, 2001. The design requirements for a module designated for use in spacecraft, boosters, and other highly rugged, conductively cooled environments are established in this standard. The requirements herein serve to specify the mechanical design of the module. Dimensions and tolerances for racks, modules, printed wiring boards, backplanes, and other connector-related dimensions that are specific to the use of 300-pin and 396-pin connectors are given. These dimensions and tolerances are designed to ensure mechanical function and interoperability.<br />\n
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          The purpose of this standard is the specification of dimensions and tolerances that will ensure the mechanical intermatability of space and highly ruggedized modules within associated subracks. Modules aspect ratios and materials/processes of current standards do not cover needs. This lack has resulted in emergence of a defacto mechanical standard for space modules, currently being produced by multiple companies. The working group will define parameters to better accommodate high dynamic mechanical stresses, limited thermal dissipation, and use of space qualifiable materials and processes. The defacto space applications standard defined by the Advanced Spaceborne Computer Module will be encompassed.
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Component
App\Twig\Components\ProductType {#93188
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          Withdrawn Standard. Withdrawn Date: Jan 15, 2001. The design requirements for a module designated for use in spacecraft, boosters, and other highly rugged, conductively cooled environments are established in this standard. The requirements herein serve to specify the mechanical design of the module. Dimensions and tolerances for racks, modules, printed wiring boards, backplanes, and other connector-related dimensions that are specific to the use of 300-pin and 396-pin connectors are given. These dimensions and tolerances are designed to ensure mechanical function and interoperability.<br />\n
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          The purpose of this standard is the specification of dimensions and tolerances that will ensure the mechanical intermatability of space and highly ruggedized modules within associated subracks. Modules aspect ratios and materials/processes of current standards do not cover needs. This lack has resulted in emergence of a defacto mechanical standard for space modules, currently being produced by multiple companies. The working group will define parameters to better accommodate high dynamic mechanical stresses, limited thermal dissipation, and use of space qualifiable materials and processes. The defacto space applications standard defined by the Advanced Spaceborne Computer Module will be encompassed.
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ProductMostRecent App\Twig\Components\ProductMostRecent 68.0 MiB 0.89 ms
Input props
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          Withdrawn Standard. Withdrawn Date: Jan 15, 2001. The design requirements for a module designated for use in spacecraft, boosters, and other highly rugged, conductively cooled environments are established in this standard. The requirements herein serve to specify the mechanical design of the module. Dimensions and tolerances for racks, modules, printed wiring boards, backplanes, and other connector-related dimensions that are specific to the use of 300-pin and 396-pin connectors are given. These dimensions and tolerances are designed to ensure mechanical function and interoperability.<br />\n
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Component
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          Withdrawn Standard. Withdrawn Date: Jan 15, 2001. The design requirements for a module designated for use in spacecraft, boosters, and other highly rugged, conductively cooled environments are established in this standard. The requirements herein serve to specify the mechanical design of the module. Dimensions and tolerances for racks, modules, printed wiring boards, backplanes, and other connector-related dimensions that are specific to the use of 300-pin and 396-pin connectors are given. These dimensions and tolerances are designed to ensure mechanical function and interoperability.<br />\n
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          This standard establishes the design requirements for a module designated for use in spacecraft, boosters, and other highly rugged, conductively cooled environments. The requirements herein serve to specify the mechanical design of the module.<br />\n
          The purpose of this standard is the specification of dimensions and tolerances that will ensure the mechanical intermatability of space and highly ruggedized modules within associated subracks. Modules aspect ratios and materials/processes of current standards do not cover needs. This lack has resulted in emergence of a defacto mechanical standard for space modules, currently being produced by multiple companies. The working group will define parameters to better accommodate high dynamic mechanical stresses, limited thermal dissipation, and use of space qualifiable materials and processes. The defacto space applications standard defined by the Advanced Spaceborne Computer Module will be encompassed.
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ProductState App\Twig\Components\ProductState 74.0 MiB 0.21 ms
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