ISO 27875:2019
Space systems — Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages — Amendment 1: Formula to obtain Ec by the product of the probability of impact on a specific latitud

Standard No.
ISO 27875:2019
Release Date
2019
Published By
International Organization for Standardization (ISO)
Status
Replace By
ISO 27875:2019/Amd 1:2020
Latest
ISO 27875:2019/Amd 1:2020
Scope
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.

ISO 27875:2019 Referenced Document

  • ISO 10795 Space systems — Programme management and quality — Vocabulary*2019-07-12 Update
  • ISO 14620-1 Space systems - Safety requirements - Part 1: System safety
  • ISO 17666 Space systems - Risk management
  • ISO 24113 Space systems — Space debris mitigation requirements*2023-05-01 Update

ISO 27875:2019 history

  • 2020 ISO 27875:2019/Amd 1:2020 Space systems — Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages — Amendment 1: Formula to obtain Ec by the product of the probability of impact on a specific latitud
  • 2019 ISO 27875:2019 Space systems — Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages — Amendment 1: Formula to obtain Ec by the product of the probability of impact on a specific latitud
  • 2016 ISO 27875:2010/Amd 1:2016 Space systems - Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages; Amendment 1
  • 2010 ISO 27875:2010 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 — Amendment 1: Formula to obtain Ec by the product of the probability of impact on a specific latitud



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