ISO 15863:2003

This standard was last reviewed and confirmed in 2020. Therefore this version remains current.

Abstract

The purpose of ISO 15863:2003 is to provide spacecraft (SC) and launch vehicle (LV) organizations with the general format for presenting the interface control document (ICD) that verifies and controls the compatibility between SC and LV for a dedicated mission. ISO 15863:2003 addresses the definition of the mission, the compatibility of the SC with the LV environment, including all mechanical, electrical, radio frequency, and electromagnetic aspects related to SC to LV and SC to launch range interfaces, verification analyses and tests for the induced environment, and the necessary facilities and support for launch range operations.

General information

Status
: Published

Publication date
: 2003-11
Edition
: 1

Number of pages
: 28
Technical Committee
: ISO/TC 20/SC 14 Space systems and operations
ICS
:
49.140 Space systems and operations

This standard contributes to the following Sustainable Development Goal:

Industry, Innovation and Infrastructure

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	Format	Language
std 1 145	PDF
std 2 145	Paper

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Life cycle

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Published

ISO 15863:2003

A standard is reviewed every 5 years
Stage: 90.93 (Confirmed)

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