BSI BS ISO 8913 Aerospace - Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400 °F/3 000 psi (204 °C/20 684 kPa) and 204 °C/21 000 kPa (400 °F/3 046 psi) - Procurement specification
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Данный раздел/документ содержится в продуктах:
Данный раздел/документ содержится в продуктах:
- Техэксперт: Машиностроительный комплекс
- Картотека зарубежных и международных стандартов
- CEN EN 2997-007 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures -65°C to 175°C continuous, 200°C continuous, 260°C peak - Part 007: Hermetic receptacle with round flange attached by welding or brazing - Product standard
- DIN EN 2997-002 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 002: Specification of performance and contact arrangements
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- CEN EN 2997-007 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures -65°C to 175°C continuous, 200°C continuous, 260°C peak - Part 007: Hermetic receptacle with round flange attached by welding or brazing - Product standard
- DIN EN 2997-002 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 002: Specification of performance and contact arrangements
- 49.060
- CEN EN 2997-007 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures -65°C to 175°C continuous, 200°C continuous, 260°C peak - Part 007: Hermetic receptacle with round flange attached by welding or brazing - Product standard
- DIN EN 2997-002 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 002: Specification of performance and contact arrangements
- CEN EN 2997-014 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 014: Square flange receptacle with integrated accessory - Product standard
- DIN EN 2997-002 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 002: Specification of performance and contact arrangements
- CEN EN 2997-007 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures -65°C to 175°C continuous, 200°C continuous, 260°C peak - Part 007: Hermetic receptacle with round flange attached by welding or brazing - Product standard
- CEN EN 2997-014 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 014: Square flange receptacle with integrated accessory - Product standard
- DIN EN 2997-002 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 002: Specification of performance and contact arrangements
- CEN EN 2997-007 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures -65°C to 175°C continuous, 200°C continuous, 260°C peak - Part 007: Hermetic receptacle with round flange attached by welding or brazing - Product standard
- CEN EN 2997-014 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 014: Square flange receptacle with integrated accessory - Product standard
- DIN EN 2997-002 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 002: Specification of performance and contact arrangements
- CEN EN 3660-002 Aerospace series - Cable outlet accessories for circular and rectangular electrical and optical connectors - Part 002: Index of product standards
- DIN EN 2997-002 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 002: Specification of performance and contact arrangements
- DIN EN 2997-002 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 002: Specification of performance and contact arrangements
- DIN EN 2997-001 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures -65 °C to 175 °C continuous, 200 °C continuous, 260 °C peak - Part 001: Technical specification
- ISO 2685 Aircraft - Environmental Test Procedure for Airborne Equipment - Resistance to Fire in Designated Fire Zones - Second Edition
- CEN EN 2997-007 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures -65°C to 175°C continuous, 200°C continuous, 260°C peak - Part 007: Hermetic receptacle with round flange attached by welding or brazing - Product standard
- Картотека зарубежных и международных стандартов
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- В списке элементов: 13
- ISO 6772 Aerospace - Fluid systems - Impulse testing of hydraulic hose, tubing and fitting assemblies - Third EditionКосмос - Жидкие системы - Импульсное испытание гидравлического шланга, трубки и подходящих сборок - Третий Выпуск
Карточка документа - ISO 2859-1 AMD 1 Sampling procedures for inspection by attributes — Part 1: Sampling schemes indexed by acceptance quality limit (AQL) for lot-by-lot inspection AMENDMENT 1 - First EditionВыборка процедур для проверки признаками — Часть 1: Выборка схем, внесенных в указатель качественным лимитом принятия (AQL) для ПОПРАВКИ 1 проверки партии по жребию - Первый Выпуск
Карточка документа - BSI BS 3TA 11 Specification for bar and section for machining of titanium-aluminium-vanadium alloy (Tensile strength 900–1 160 MPa) (Limiting ruling section 150 mm)Спецификация для бара и секция для машинной обработки ванадиевого алюминием титаном сплава (Прочность на растяжение 900–1 160 МПа) (Ограничение управляющего раздела 150 mm)
Карточка документа - CEN EN 9100 Quality Management Systems - Requirements for Aviation, Space and Defense OrganizationsСистемы управления качеством - требования для авиации, пространства и организаций защиты
На основе CEN EN 9100 разработан ГОСТ Р ЕН 9100-2011 (IDT)ГОСТ Р ЕН 9100-2011 (IDT) - ISO 8829-2 Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 2: Non-metallic braid - First Edition;:1990Космические Методы испытаний для polytetrafluoroethylene (PTFE) сборочная Часть 2 шланга камеры: неметаллическая оплетка - Первый Выпуск;:1990
Карточка документа - CEN EN 9133 Aerospace series - Quality management systems - Qualification procedure for aerospace standard partsКосмический ряд - Системы управления качеством - процедура Квалификации для космических стандартных частей
Карточка документа - ISO 3161 Aerospace - UNJ Threads - General Requirements and Limit Dimensions - Third EditionКосмос - резьба UNJ - общие требования и предельные измерения - третий выпуск
Карточка документа - ISO 5855-3 Aerospace - MJ Threads - Part 3: Limit Dimensions for Fittings for Fluid Systems - Second EditionКосмос - резьба MJ - часть 3: предельные измерения для деталей для жидких систем - второй выпуск
На основе ISO 5855-3 разработан ГОСТ 30892-2002 (MOD)ГОСТ 30892-2002 (MOD) - ISO 2685 Aircraft - Environmental Test Procedure for Airborne Equipment - Resistance to Fire in Designated Fire Zones - Second EditionСамолет - процедура испытания на воздействие окружающей среды для бортового оборудования - сопротивление для увольнения в определяемые зоны огня - второй выпуск
Карточка документа - BSI BS 3S 145 Specification for Chromium-nickel-coppermolybdenum corrosion resisting steel (precipitation hardening) billets, bars, forgings and parts (1270 MPa to 1470 MPa) - AMD 9768: February 15, 1998Спецификация для коррозии Chromium-nickel-coppermolybdenum, сопротивляющейся стали (упрочнение дисперсионными частицами) ордера на постой, бары, штамповки и части (от 1270 МПа до 1470 МПа) - AMD 9768: 15 февраля 1998
Карточка документа - ISO 7258 Polytetrafluoroethylene (PTFE) Tubing for Aerospace Applications - Methods for the Determination of the Density and Relative Density First EditionPolytetrafluoroethylene (PTFE) трубка для космических заявлений - методы для определения плотности и относительной плотности первый выпуск
Карточка документа - BSI BS 2S 130 Specification for 18/9 chromium-nickel corrosion-resisting steel (niobium stabilized) billets, bars, forgings and parts - (540 MPa: limiting ruling section 150 mm) - AMD 2640: June 1978Спецификация для 18/9 стали сопротивления коррозии никеля хрома (стабилизированный ниобий) ордера на постой, бары, штамповки и части - (540 МПа: ограничение управляющего раздела 150 mm) - AMD 2640: июнь 1978
Карточка документа - BSI BS 2S 129 Specification for 18/9 chromium-nickel corrosion-resisting steel (titanium stabilized) billets, bars, forgings and parts - (540 MPa: limiting ruling section 150 mm) - AMD 2646: July 1978Спецификация для 18/9 стали сопротивления коррозии никеля хрома (стабилизированный титан) ордера на постой, бары, штамповки и части - (540 МПа: ограничение управляющего раздела 150 mm) - AMD 2646: июль 1978
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