ISO 27875:2019
Space systems — Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages
Space systems — Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages
- Статус документа:
- Отменён
- Формат:
- Электронный (PDF)
- Количество страниц:
- 23
- Дата публикации:
- 1 февраля 2019 г.
- Издание:
- ISO IS 27875 edition 2 version 1
- ICS:
- 49.140
This document provides a framework with which to assess, reduce, and control the potential risks that spacecraft and launch vehicle orbital stages (referred to hereinafter as "space vehicles") pose to people and the environment when those space vehicles re-enter the Earth's atmosphere and impact the Earth's surface. It is intended to be applied to the planning, design, and review of space vehicle missions for which controlled or uncontrolled re-entry is inevitable. This document is applicable to following objects in assessing their risk to the ground: a) objects re-entering from orbit in conformance with ISO 24113; b) launch vehicles (including payloads, other objects separated during the ascent phase, etc.) that are mentioned in flight safety activities under ISO 14620‑2[1]; and c) interplanetary spacecraft returning to Earth. This document complements ISO 14620‑1 and ISO 17666. This document is not applicable to spacecraft containing nuclear power sources[2]. NOTE 1 This document does not apply to Space Transportation Systems with wings and control functions intended for targeted landing. NOTE 2 Useful background information for this document is available in ISO 24113.
Abstract
Overview
ISO 27875:2019 - Space systems - Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages - defines a framework to assess, reduce, and control risks posed to people and the environment when unmanned space vehicles re‑enter the Earth’s atmosphere. It covers both natural (uncontrolled) and controlled re‑entry scenarios and is intended for use during planning, design, review and operations for missions where re‑entry is inevitable. The standard explicitly excludes spacecraft with nuclear power sources and winged systems intended for targeted landing.
Key technical topics and requirements
- Re‑entry safety programme: Establish and maintain a programme to minimise casualties and environmental damage; integrate with system safety activities.
- Re‑entry Risk Assessment and Mitigation Plan (RRAMP): Prepare, update and obtain authorization for a RRAMP as part of the safety data package. Annex A lists typical RRAMP contents.
- Organizational oversight: Appoint safety representatives with authority to access data, halt activities or reject documents; conduct phase reviews and manage waivers/deviations.
- Risk assessment methods:
- Natural re‑entry: Estimate the expected number of casualties (Ec) using casualty-area, orbital inclination and population density (Annex C describes calculation guidance). For natural re‑entry the likelihood is treated as 1.0 and risk is driven by Ec.
- Controlled re‑entry: Plan landing area, design features, contingency notifications and post‑re‑entry activities; perform specific risk assessments and non‑conformance handling.
- Risk‑reduction measures:
- Design measures to reduce survivability of debris on re‑entry.
- Operational measures including controlled re‑entry planning, designated impact areas (typically uninhabited).
- Environmental risk assessment: Assess ground pollution potential and include mitigation in RRAMP.
- Documentation and process: Follow ISO 17666 risk‑management process (Annex B) and retain traceable records for reviews and authorization.
Practical applications and users
ISO 27875:2019 is practical for:
- Spacecraft and launch vehicle designers and manufacturers
- Satellite operators and mission planners
- Launch service providers and range safety teams
- Safety engineers and programme managers preparing RRAMPs
- National safety authorities and regulators overseeing re‑entry compliance
Use cases include mission design reviews, end‑of‑life disposal planning, contingency planning for re‑entry events, and establishing organizational safety oversight.
Related standards
- ISO 24113 - Space debris mitigation requirements (background and complementary guidance)
- ISO 14620‑1 / ISO 14620‑2 - System safety and flight safety activities
- ISO 17666 - Risk management process and principles
Keywords: ISO 27875:2019, re‑entry risk management, spacecraft re‑entry, launch vehicle orbital stages, RRAMP, expected number of casualties, controlled re‑entry, natural re‑entry, space systems safety.
Технические детали
- Технический комитет
- ISO/TC 20/SC 14 - Space systems and operations
- SKU
- ISO 27875:2019
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