ISO 16458:2004 PDF

Name: ISO 16458:2004 — Space systems — Unmanned spacecraft transportation — General requirements
SKU: ISO 16458:2004
Price: 25 EUR
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Space systems — Unmanned spacecraft transportation — General requirements

Название (английский):

ISO 16458:2004

Space systems — Unmanned spacecraft transportation — General requirements

Статус документа:: Действующий
Формат:: Электронный (PDF)
Количество страниц:: 8
Дата публикации:: 6 января 2004 г.
Издание:: ISO IS 16458 edition 1 version 1
ICS:: 49.140

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Описание (английский):

ISO 16458:2004 is applicable to unmanned spacecraft and their supporting hardware including science instrument and payloads. It establishes the requirements for transportation by rail, road, air, and water and as a part of a launch vehicle and establishes the requirements for special containers and loading/unloading operations meant to safeguard unmanned spacecraft and their supporting hardware during transportation. ISO 16458:2004 is intended to be applied in international transportation. It may also be used in national transportation.

Abstract

Похожие стандарты

Стандарты, упомянутые в описании

Overview

ISO 16458:2004 - Space systems - Unmanned spacecraft transportation - General requirements - defines general requirements for the safe international transportation of unmanned spacecraft (SC) and their supporting hardware, including science instruments and payloads. The standard covers transportation by rail, road, air and water, transportation as part of a launch vehicle, plus requirements for special shipping containers, loading/unloading operations, and operational documentation (OD) needed to safeguard spacecraft during transit.

Key topics and technical requirements

Scope and applicability: Unmanned spacecraft, major components, support equipment and spare parts; intended primarily for international transport but usable for national movements.

Operational documentation (OD): Transport modes, environmental limits, mechanical load limits and inspection procedures must be specified in the OD prepared by the spacecraft developer.

Container design:

Dust- and moisture-tight construction; protection against water penetration and contaminants
Environmental control targets (example ranges given: temperature −50 °C to +50 °C unless OD specifies otherwise; relative humidity ≤ 60 % or per OD)
Pressure equalization and, for thermal containers, typical pressure range (93–113 kPa) and air cleanliness per OD
Shock-absorption systems to reduce transport loads when required
RF shielding where SC is RF-sensitive; corrosion resistance; materials compatible with propellants and clean-room entry

Monitoring & recording: Remote monitoring and shock-recording sensors integrated into containers when required by OD; defined permissible ranges to be recorded.

Safety controls: Electrical grounding during transport, pyrotechnic items rendered safe/inactive, compliance with UN and national transport safety regulations.

Mode-specific rules:

Rail: prohibit humping, strict speed/approach limits and external inspections en route
Road: pre-movement checks, inspections at defined intervals (e.g., ~1–1.5 km after start and every ~150 km, unless OD specifies otherwise)
Air: inspections before takeoff and after landing; aircraft must withstand expected static/vibration loads and pressure differentials
Water: secure tie-downs, protection from seawater, tie-down inspections at least four times per 24 h (first within 0.5–1 h)

Practical applications and who uses it

Who: spacecraft manufacturers, launch service providers, systems integrators, payload suppliers, transport/logistics contractors, ground handling teams, safety officers, and regulatory compliance personnel.

Use cases:

Designing and qualifying spacecraft shipping containers and shock-absorption systems
Writing transport plans and operational documentation (OD) with environmental and load limits
Specifying contractual and inspection requirements for carriers and escorts
Ensuring safety and regulatory compliance for international shipment of spacecraft hardware

Related standards

ISO 14303 - Space systems - Launch-vehicle-to-spacecraft interfaces

ISO 15863 - Space systems - Spacecraft-to-launch-vehicle interface control document

ISO 17401 - Space systems - Documents for spacecraft interface requirements for launch vehicle services

Keywords: ISO 16458, unmanned spacecraft transportation, spacecraft shipping containers, transport requirements, shock absorption, moisture control, RF shielding, launch vehicle transport, international spacecraft logistics.

ISO 16458:2004 PDF

Abstract

Похожие стандарты

Overview

Key topics and technical requirements

Practical applications and who uses it

Related standards

Технические детали

BS ISO 14303:2002

Space systems. Launch-vehicle-to-spacecraft interfaces.

BS ISO 15863:2003

Space systems. Spacecraft-to-launch-vehicle interface control document.

ISO 1740:1991

Milk fat products and butter — Determination of fat acidity (Reference method)