EN 16603-35-02:2014

Space engineering - Solid propulsion for spacecrafts and launchers

General requirements applying to all type of Propulsion Systems Engineering are defined in ECSS-E-ST-35. For solid propulsion activities within a space project the standards ECSS-E-ST-35 and ECSS-E-ST-35-02 are applied together.
This Standard defines the regulatory aspects that apply to the elements and processes of solid propulsion for launch vehicles and spacecraft. 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.
NOTE 1   Some solid propulsion systems use hot gas valves, for thrust or pressure modulation. The requirements applicable to these systems are not covered by the present document.
NOTE 2   For SRM with TVC, only moveable nozzle with flexseal are addressed.
This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.

Raumfahrttechnik - Feststoffantriebe für Raumfahrzeuge und Trägerraketen

Ingénierie spatiale - Propulsion solide pour satellites et lanceurs

Vesoljska tehnika - Trdna pogonska goriva za vesoljska plovila in lansirnike

Splošne zahteve, ki veljajo za vse vrste inženiringa pogonskih sistemov, so opredeljene v standardu ECSS-E-ST-35. Za dejavnosti, povezane s trdnimi pogonskimi gorivi v okviru vesoljskega projekta, skupaj veljata standarda ECSS-E-ST-35 in ECSS-E-ST-35-02. Ta standard opredeljuje regulatorne vidike, ki se nanašajo na elemente in postopke za trdna pogonska goriva za vesoljska plovila in lansirnike. Določa dejavnosti, ki se izvajajo v tehničnem delu teh pogonskih sistemov in njihovo uporabnost. Določa zahteve za tehnične vidike, kot so funkcionalni, fizikalni, okoljski, kakovostni dejavniki, zahteve med delovanjem in verifikacijo.

General Information

• Status: Published
• Publication Date: 09-Sep-2014
• Withdrawal Date: 30-Mar-2015
• ICS: 49.140 - Space systems and operations
• Technical Committee: CEN/CLC/TC 5 - Space
• Drafting Committee: CEN/CLC/TC 5 - Space
• Current Stage: 9060 - Closure of 2 Year Review Enquiry - Review Enquiry
• Start Date: 03-Mar-2020
• Completion Date: 03-Mar-2020
• Mandate: M/496 - Mandate addressed to CEN, CENELEC and ETSI to develop standardisation regarding space industry (Phase 3 of the process)
• Ref Project: SIST EN 16603-35-02:2014 - Space engineering - Solid propulsion for spacecrafts and launchers

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Vesoljska tehnika - Trdna pogonska goriva za vesoljska plovila in lansirnikeRaumfahrttechnik - Feststoffantriebe für Raumfahrzeuge und TrägerraketenIngénierie spatiale - Propulsion solide pour satellites et lanceursSpace engineering - Solid propulsion for spacecrafts and launchers49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 16603-35-02:2014SIST EN 16603-35-02:2014en,fr,de01-november-2014SIST EN 16603-35-02:2014SLOVENSKI
STANDARD



SIST EN 16603-35-02:2014



EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16603-35-02
September 2014 ICS 49.140
English version
Space engineering - Solid propulsion for spacecrafts and launchers
Ingénierie spatiale - Propulsion solide pour satellites et lanceurs
Raumfahrttechnik - Feststoffantriebe für Raumfahrzeuge und Trägerraketen This European Standard was approved by CEN on 23 February 2014.
CEN and CENELEC members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN and CENELEC member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN and CENELEC member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions.
CEN and CENELEC members are the national standards bodies and national electrotechnical committees of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom.
CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels © 2014 CEN/CENELEC All rights of exploitation in any form and by any means reserved worldwide for CEN national Members and for CENELEC Members. Ref. No. EN 16603-35-02:2014 E SIST EN 16603-35-02:2014



EN 16603-35-02:2014 (E) 2 Table of contents Foreword . 4 Introduction . 5 1 Scope . 6 2 Normative references . 7 3 Terms, definition and abbreviated terms . 8 3.1 Terms from other standards . 8 3.2 Abbreviated terms. 9 4 Solid propulsion engineering activities . 10 4.1 Overview . 10 4.2 Functional . 10 4.2.1 Mission . 10 4.2.2 Functions . 10 4.3 Constraints . 12 4.3.1 Dynamic phenomena . 12 4.3.2 External loads during the life cycle of the propulsion system . 12 4.3.3 Thrust centroid time . 12 4.3.4 Acoustic noise . 12 4.3.5 Pollution . 12 4.3.6 Ejected parts . 13 4.3.7 Safety. 13 4.4 Interfaces . 13 4.4.1 General
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