Space systems — Spacecraft interface requirements document for launch vehicle services

This document provides spacecraft (SC) organizations with the general format for presenting the interface requirement document (IRD) for launch vehicle services. The IRD provides a list of the major technical requirements spacecraft agencies provide to launch vehicle (LV) agencies when submitting an application for launch services. The IRD addresses the definition of the SC mission, the mechanical and electrical interfaces, the overall environment requirements (mechanical, thermal, cleanliness, radio-electrical), the SC development and test programme and, finally, launch range facilities and support requirements. This document is applicable to all existing commercial LV and related launch facilities so as to permit SC contractors to prepare a single interface requirement document for a given SC mission, independently of the LV contractor to be selected. The IRD, as defined in this document, includes the basic SC input data needed by LV agencies to prepare the interface control document defined in ISO 15863.

Systèmes spatiaux — Document d'exigences d'interface du véhicule spatial vis-à-vis du service de lancement

General Information

Status
Published
Publication Date
04-May-2023
Current Stage
6060 - International Standard published
Start Date
05-May-2023
Due Date
08-Jul-2022
Completion Date
05-May-2023
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Relations

Standard
ISO 17401:2023 - Space systems — Spacecraft interface requirements document for launch vehicle services Released:5. 05. 2023
English language
23 pages
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Standards Content (Sample)


INTERNATIONAL ISO
STANDARD 17401
Second edition
2023-05
Space systems — Spacecraft interface
requirements document for launch
vehicle services
Systèmes spatiaux — Document d'exigences d'interface du véhicule
spatial vis-à-vis du service de lancement
Reference number
© ISO 2023
All rights reserved. Unless otherwise specified, or required in the context of its implementation, no part of this publication may
be reproduced or utilized otherwise in any form or by any means, electronic or mechanical, including photocopying, or posting on
the internet or an intranet, without prior written permission. Permission can be requested from either ISO at the address below
or ISO’s member body in the country of the requester.
ISO copyright office
CP 401 • Ch. de Blandonnet 8
CH-1214 Vernier, Geneva
Phone: +41 22 749 01 11
Email: copyright@iso.org
Website: www.iso.org
Published in Switzerland
ii
Contents Page
Foreword .v
Introduction . vi
1 Scope . 1
2 Normative references . 1
3 Terms, definitions and abbreviated terms . 1
3.1 Terms and definitions . 1
3.2 Abbreviated terms . 1
4 Spacecraft mission description .2
4.1 Mission description . 2
4.2 SC description (optional) . 2
5 Mechanical interfaces. 2
5.1 Mechanical configuration . 2
5.2 SC fundamental frequencies . 2
5.3 Usable volume. 3
5.4 Spacecraft (or SC adapter) mechanical interface . 3
5.5 Connectors and microswitches (SC side of the interface) . 3
5.6 Purges and fluid connection interface . 4
5.7 Encapsulated spacecraft access . 4
6 Electrical interfaces .4
6.1 Umbilical wiring diagram . 4
6.2 Umbilical connectors . 4
6.3 Umbilical wiring links (for each connector pin) . 5
6.4 Electrical commands dedicated to spacecraft . 5
6.4.1 Pyrotechnic commands . . 5
6.4.2 Dry loop commands . 6
6.4.3 Electrical commands . 6
6.5 Separation status transmission . 7
6.6 SC in-flight telemetry . 7
6.7 Power supply required from LV . 7
6.8 Earth potential continuity . 7
7 Radio-frequency and electromagnetic interface . 8
7.1 Characteristics of radio-electrical systems . 8
7.2 RF telemetry and command link . 9
7.2.1 SC RF-link definition for ground operations . 9
7.2.2 SC antenna coordinates . 9
7.2.3 RF-link implementation . 9
7.2.4 RF-link budget . 9
7.2.5 Base band signal characteristics . 10
8 Spacecraft mission characteristics .11
8.1 SC input data for mission analyses . 11
8.1.1 Mass and inertia characteristics . 11
8.1.2 Sloshing masses (pendulum-type) . 11
8.1.3 SC mission constraints (when applicable) .12
8.2 SC orbit parameters (with tolerances) .12
8.3 Launch window .13
8.3.1 Launch window constraints (when applicable) .13
8.3.2 Preferred window .13
8.4 SC pointing and separation . . .13
9 Environment requirements .13
9.1 General .13
9.2 Mechanical environment .13
iii
9.3 Thermal environment . 14
9.4 Static pressure . 14
9.5 Contamination and cleanliness control . 15
9.6 Radio frequency and electromagnetic environment . 15
9.7 Environment monitoring . 15
9.8 Exposure to sun . 15
10 SC Development and test programme .15
10.1 Mechanical environment qualification tests . 15
10.2 LV/SC compatibility tests . 16
11 Launch range operations: facilities and support requirements .16
11.1 General logistics requirements . 16
11.1.1 General . 16
11.1.2 SC container and ground support equipment physical envelopes . 16
11.1.3 Material handling equipment . . 17
11.1.4 Electrical power for SC and ground station . 17
11.1.5 Umbilical lines and ground lines . 17
11.1.6 Gas and fluid lines . 17
11.1.7 Clean room . 18
11.1.8 Environmental controls for SC and ground station . 18
11.1.9 Clothing (safety and cleanroom) . 18
11.1.10 Area . 18
11.1.11 Storage (non-hazardous items) . 19
11.1.12 SC pre-launch activities calendar . 19
11.1.13 Special technical support equipment . 19
11.1.14 Other . 19
11.2 Specific requirements for solid propellant motor facilities (Y/N, to specify) .
...

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