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EN 16603-35-03:2014

Current

Current

The latest, up-to-date edition.

Space engineering - Liquid propulsion for launchers

Published date

09-10-2014

Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
4 Overview of a liquid propulsion system
5 Functional
6 Constraints
7 Development
8 Interfaces
9 Design
10 Ground support equipment
11 Materials
12 Verification
13 Production and manufacturing
14 In-service
15 Deliverables
Bibliography

General requirements applying to all type of Propulsion Systems Engineering are defined in ECSS-E-ST-35. For Liquid propulsion for launchers activities within a space project the standards ECSS-E-ST-35 and ECSS-E-ST-35-03 are applied together.This Standard defines the specific regulatory aspects that apply to the elements and processes of liquid propulsion for launch vehicles. It specifies the activities to be performed in the engineering of these propulsion systems and their applicability. It defines the requirements for the engineering aspects such as functional, physical, environmental, quality factors, operational and verification.Other forms of propulsion (e.g. nuclear, nuclear-electric, solar-thermal and hybrid propulsion) are not presently covered in this issue of the Standard.This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.

Committee
CEN/CLC/JTC 5
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Current

BS EN 16603-35:2014 Space engineering. Propulsion general requirements
I.S. EN 16603-35:2014 SPACE ENGINEERING - PROPULSION GENERAL REQUIREMENTS
I.S. EN 16603-35-02:2014 SPACE ENGINEERING - SOLID PROPULSION FOR SPACECRAFTS AND LAUNCHERS
EN 16603-35-02:2014 Space engineering - Solid propulsion for spacecrafts and launchers
EN 16603-35:2014 Space engineering - Propulsion general requirements
BS EN 16603-35-02:2014 Space engineering. Solid propulsion for spacecrafts and launchers

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