ISO 5879:2023
Space systems — Ground test for the separation between a launch vehicle and a spacecraft — Requirements for combined separation tests, horizontal separation tests and individual falling separation tests
Space systems — Ground test for the separation between a launch vehicle and a spacecraft — Requirements for combined separation tests, horizontal separation tests and individual falling separation tests
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 32
- Дата публикации:
- 14 августа 2023 г.
- Издание:
- ISO IS 5879 edition 1 version 1
- ICS:
- 49.140
This document provides the test requirements of three typical separation test methods, which are the combined separation test, the horizontal separation test, the individual falling separation test, for the separation between the launch vehicle (LV) and the spacecraft (or between stages of a prototype LV model). It also provides the requirements for the separation test unit, test data, test timing and sequence, pre-test simulation, test environment, exception handling, test results assessment, test documentation, test facilities, test installation, preliminary adjustment of the test setup, measurement and data acquisition. This document is applicable to test providers and interested parties to implement the separation test between the launch vehicle and the spacecraft.
Abstract
Overview
ISO 5879:2023 - "Space systems - Ground test for the separation between a launch vehicle and a spacecraft" - defines requirements for ground separation tests used to verify and diagnose separation events between a launch vehicle (LV) and a spacecraft, or between stages of a prototype LV model. The standard covers three primary test methods: combined separation tests, horizontal separation tests, and individual falling separation tests, and specifies requirements for test units, data, timing, pre-test simulation, test environment, exception handling, results assessment and documentation.
Keywords: ISO 5879:2023, space systems, separation test, launch vehicle, spacecraft, ground test, combined separation test, horizontal separation test, individual falling separation test.
Key topics and technical requirements
- Test methods: Prescriptive requirements for combined, horizontal and individual falling separation tests and their interdependencies (informative annexes explain implementation).
- Separation test unit & test articles: Definition and specification of the test hardware, installation, functional constraints and technical safety requirements.
- Measurement & instrumentation: Requirements for accelerometers (translational & shock), rate gyroscopes, high‑speed video, timing systems, optical displacement systems and shock measurement systems.
- Test facilities & fixtures: Calibration, control instrumentation (power, release mechanism controllers), test scaffolding, angular rotation mechanisms, release mechanisms and capture systems.
- Pre-test simulation: Modelling, solver and validation requirements to support test planning and result interpretation.
- Data requirements & acquisition: Types of required test data (separation movement, shock response, dedicated dataset), data formats, noise reduction, SRS (shock response spectrum) reporting and anomaly detection.
- Test timing, sequencing & exception handling: Guidance on sequencing, permitted interruptions and handling abnormal events during test execution.
- Results assessment & documentation: Criteria for evaluating outcomes, required documentation, and archiving of test results and records.
Practical applications and who uses it
ISO 5879:2023 is intended for:
- Test providers and ground test facilities performing separation verification.
- Launch vehicle and spacecraft manufacturers conducting qualification and acceptance tests.
- Systems engineers and test engineers responsible for test planning, instrumentation and data analysis.
- Safety and quality assurance teams ensuring compliance and traceability of separation tests.
Use cases include qualification of separation systems, verification of pyrotechnic or mechanical release mechanisms, and validation of separation dynamics during design and integration.
Related standards (if applicable)
ISO 5879 references normative documents and aligns with broader space systems testing standards and facility calibration and measurement best practices. For implementation, review the normative references listed within ISO 5879:2023 and consult relevant national or industry standards for complementary requirements.
Технические детали
- Технический комитет
- ISO/TC 20/SC 14 - Space systems and operations
- SKU
- ISO 5879:2023
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