EN 16603-35-03:2014
(Main)Space engineering - Liquid propulsion for launchers
Space engineering - Liquid propulsion for launchers
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.
Raumfahrttechnik - Flüssigantriebe für Trägerraketen
Ingénierie spatiale - Propulsion liquide pour lanceurs
Vesoljska tehnika - Tekoča pogonska goriva za lansirnike
Splošne zahteve, ki veljajo za vse vrste inženiringa pogonskih sistemov, so opredeljene v standardu ECSS-E-ST-35. Za dejavnosti, povezane s tekočimi pogonskimi gorivi v okviru vesoljskega projekta, skupaj veljata standarda ECSS-E-ST-35 in ECSS-E-ST-35-02. Ta standard opredeljuje posebne regulatorne vidike, ki se nanašajo na elemente in postopke za tekoča pogonska goriva za lansirnike. Določa dejavnosti, ki se izvajajo v tehničnem delu teh pogonskih sistemov in njihovo uporabnost. Določa zahteve za inženirske vidike, kot so funkcionalni, fizikalni, okoljski, kakovostni dejavniki, zahteve med delovanjem in verifikacijo. Druge oblike pogonov (npr. jedrski, jedrsko-električni, solarno-termalni in hibridni pogon) trenutno niso zajeti v tej izdaji standarda. Ta standard se lahko prilagodi posameznim lastnostim in omejitvam vesoljskega projekta v skladu s standardom ECSS-S-ST-00.
General Information
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Raumfahrttechnik - Flüssigantriebe für TrägerraketenIngénierie spatiale - Propulsion liquide pour lanceursSpace engineering - Liquid propulsion for launchers49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 16603-35-03:2014SIST EN 16603-35-03:2014en,fr,de01-november-2014SIST EN 16603-35-03:2014SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16603-35-03
September 2014 ICS 49.140
English version
Space engineering - Liquid propulsion for launchers
Ingénierie spatiale - Propulsion liquide pour lanceurs
Raumfahrttechnik - Flüssigantriebe für 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 16603-35-03:2014 E SIST EN 16603-35-03:2014
This standard forms parts of ECSS-E-ST-35 series which has the following structure; • ECSS-E-ST-35 Propulsion general requirements • ECSS-E-ST-35-01
Liquid and electric propulsion for spacecrafts • ECSS-E-ST-35-02 Solid propulsion for spacecrafts and launchers • ECSS-E-ST-35-03 Liquid propulsion for launchers • ECSS-E-ST-35-06 Cleanliness requirements for spacecraft propulsion components, subsystems, and systems • ECSS-E-ST-35-10 Compatibility testing for liquid propulsion components, subsystems, and systems ECSS-E-ST-35 contains all the normative references, terms, definitions, abbreviated terms, symbols and DRD that are applicable for ECSS-E-ST-35, ECSS-E-ST-35-01, ECSS-E-ST-35-02 and ECSS-E-ST-35-03. In the use of this standard, the term ‘propulsion system’ is intended to be read and interpreted only and specifically for ‘liquid prolusion system’. SIST EN 16603-35-03:2014
EN reference Reference in text Title EN 16601-00-01 ECSS-S-ST-00-01 ECSS system - Glossary of terms
EN 16603-10 ECSS-E-ST-10 Space engineering - System engineering general requirements EN 16603-10-02 ECSS-E-ST-10-02 Space engineering - Verification EN 16603-10-06 ECSS-E-ST-10-06 Space engineering - Technical requirements specification EN 16603-32 ECSS-E-ST-32 Space engineering - Structural general requirements EN 16603-32-02 ECSS-E-ST-32-01 Space engineering - Fracture control EN 16603-32-02 ECSS-E-ST-32-02 Space engineering - Structural design and verification of pressurized hardware EN 16603-32-10 ECSS-E-ST-32-10 Space engineering - Structural factors of safety for spaceflight hardware EN 16603-35 ECSS-E-ST-35 Space engineering - Propulsion general requirements EN 16602-70 ECSS-Q-ST-70 Space product assurance - Materials, mechanical parts and processes
ISO 15389:2001 Space systems - Flight-to-ground umbilicals
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