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Space systems — Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages
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.
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