iTeh StandardsiTeh Standards
EURUSD
Your shopping cart is empty.
SIST

SIST EN 14607-6:2005

(Main)

Space engineering - Mechnical - Part 6: Pryotechnics

Space engineering - Mechnical - Part 6: Pryotechnics

EN 14607 Part 6 of Space engineering - Mechanical defines the requirements for the discipline of pyrotechnics engineering.
This part defines the standards to be applied for the use of pyrotechnics on all spacecraft and other space products including launch vehicles. It addresses the aspects of design, analysis, verification, manufacturing, operations and safety.
As any pyrotechnic item used for flight can function only once, it can never be fully tested before its crucial mission operation. The required confidence can only be established indirectly by the testing of identical items. Test results and theoretical justification are essential for demonstration of fulfilment of the requirements. The requirement for repeatability shows that product assurance plays a crucial role in support of technical aspects.
The failure or unintentional operation of a pyrotechnic item can be catastrophic for the whole mission and life threatening. Specific requirements can exist for the items associated with it. As all pyrotechnic functions are to be treated similarly, collective control needs to be applied in the manner of a subsystem.
When viewed from the perspective of a specific project context, the requirements defined in this document should be tailored to match the genuine requirements of a particular profile and circumstances of a project.
NOTE   Tailoring is a process by which individual requirements of specifications, standards and related documents are evaluated, and made applicable to a specific project by selection, and in some exceptional cases, modification of existing or addition of new requirements.

Raumfahrttechnik - Mechanik - Teil 6: Pyrotechnik

Ingénierie spatiale - Mécanique - Partie 6: Pyrotechnie

Vesoljska tehnika – Mehanika – 6. del: Pirotehnika

General Information

Status
Withdrawn
Publication Date
31-Dec-2004
Withdrawal Date
24-Apr-2019
ICS
49.140 - Space systems and operations
Technical Committee
I13 - Imaginarni 13
Current Stage
9900 - Withdrawal (Adopted Project)
Start Date
25-Apr-2019
Due Date
18-May-2019
Completion Date
25-Apr-2019
Mandate
M/237 - Mandate to CEN, CENELEC and ETSI for standardization in the field of equipment for the space industry
Ref Project
EN 14607-6:2004 - Space engineering - Mechanical - Part 6: Pyrotechnics

Relations

Replaced By
SIST EN 16603-33-11:2019 - Space engineering - Explosive subsystems and devices
Effective Date
24-Apr-2019
Revised
SIST EN 16603-33-11:2019 - Space engineering - Explosive subsystems and devices
Effective Date
13-Jun-2018

Buy Standard

EN 14607-6:2005EN 14607-6:2005
PreviousNext
Standard
EN 14607-6:2005
English language
33 pages
sale 10% off
Preview
sale 10% off
Preview
e-Library read for
1 day

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Vesoljska tehnika – Mehanika – 6. del: PirotehnikaRaumfahrttechnik - Mechanik - Teil 6: PyrotechnikIngénierie spatiale - Mécanique - Partie 6: PyrotechnieSpace engineering - Mechnical - Part 6: Pryotechnics49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 14607-6:2004SIST EN 14607-6:2005en01-januar-2005SIST EN 14607-6:2005SLOVENSKI
STANDARD



SIST EN 14607-6:2005



SIST EN 14607-6:2005



SIST EN 14607-6:2005



SIST EN 14607-6:2005



SIST EN 14607-6:2005



SIST EN 14607-6:2005



SIST EN 14607-6:20
...

Questions, Comments and Discussion

Ask us and Technical Secretary will try to provide an answer. You can facilitate discussion about the standard in here.

This May Also Interest You

SIST
SIST EN 16602-60-13:2023(Main)
Space product assurance - Commercial electrical, electronic and electromechanical (EEE) components
EN 16602-60-13:2023

2021-04-21: This EN is based on ECSS-Q-ST-60-13C Rev.1

  • Standard
    106 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    123 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 16602-70-40:2023(Main)
Space product assurance - Processing and quality assurance requirements for hard brazing of metallic materials for flight hardware
EN 16602-70-40:2023

2021-04-21: This EN is based on ECSS-Q-ST-70-40C

  • Standard
    39 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    38 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 16602-60:2023(Main)
Space product assurance - Electrical, electronic and electromechanical (EEE) components
EN 16602-60:2023

The Scope of the Standard remains unchanged.
This standard defines the requirements for selection, control, procurement and usage of EEE components for space projects.
This standard differentiates between three classes of components through three different sets of standardization requirements (clauses) to be met.
The three classes provide for three levels of trade-off between assurance and risk. The highest assurance and lowest risk is provided by class 1 and the lowest assurance and highest risk by class 3. Procurement costs are typically highest for class 1 and lowest for class 3. Mitigation and other engineering measures may decrease the total cost of ownership differences between the three classes. The project objectives, definition and constraints determine which class or classes of components are appropriate to be utilised within the system and subsystems.
a.   Class 1 components are described in Clause 4.
b.   Class 2 components are described in Clause 5
c.   Class 3 components are described in Clause 6.
The requirements of this document apply to all parties involved at all levels in the integration of EEE components into space segment hardware and launchers.

  • Standard
    103 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    126 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 16602-70-61:2022(Main)
Space product assurance - High-reliability soldering for surface mount, mixed technology and hand-mounted electrical connections
EN 16602-70-61:2022

This standard defines:
- the basic requirements for the verification and approval of automatic machine w ave soldering for use in spacecraft hardware. The process requirements for w ave soldering of doublesided and multilayer boards are also defined.
- the technical requirements and quality assurance provisions for the manufacture and verification of manuallysoldered, high-reliability electrical connections.
- the technical requirements and quality assurance provisions for the manufacture and verification of high-reliability electronic circuits based on surface mounted device (SMD) and mixed technology.
- the acceptance and rejection criteria for high reliability manufacture of manually-soldered electrical connections intended to w ithstand normal terrestrial conditions and the vibrational g-loads and environment imposed by space flight.
- the proper tools, correct materials, design and w orkmanshipt. Workmanship standards are included to permit discrimination betw een proper and improper work.
SCOPE
This Standard defines the technical requirements and quality assurance provisions for the manufacture and verification of high-reliability electronic circuits of surface mount, through hole and solderless assemblies.
The Standard defines w orkmanship requirements, the acceptance and rejection criteria for high-reliability assemblies intended to withstand normal terrestrial conditions and the environment imposed by space flight.
The mounting and supporting of components, terminals and conductors specified in this standard applies only to assemblies designed to continuously operate over the mission w ithin the temperature limits of -55 °C to +85 °C at solder joint level.
Requirements related to printed circuit boards are contained in ECSS-Q-ST-70-60 (equivalent to EN 16602-70-60) and ECSS-Q-ST-70-12 (equivalent to EN 16602-70-12).
This Standard does not cover the qualification and acceptance of the EQM and FM equipment w ith high-reliability electronic circuits of surface mount, through hole and solderless assemblies.
This Standard does not cover verification of thermal properties for component assembly.
This Standard does not cover pressfit connectors.
The qualification and acceptance tests of equipment manufactured in accordance w ith this Standard are covered by ECSS-EST-10-03 (equivalent to EN 16603-10-03).

  • Standard
    253 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    247 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 16603-20-07:2022(Main)
Space engineering - Electromagnetic compatibility
EN 16603-20-07:2022

EMC policy and general system requirements are specified in ECSS-E-ST-20 (equivalent to EN 16603-20).
This ECSS-E-ST-20-07 (equivalent to EN 16603-20-07) Standard addresses detailed system requirements (Clause 4), general test conditions, verification requirements at system level, and test methods at subsystem and equipment level (Clause 5) as w ell as informative limits (Annex A).
Associated to this standard is ECSS-E-ST-20-06 (equivalent to EN 16603-20-06) "Spacecraft charging", w hich addresses charging control and risks arising from environmental and vehicle-induced spacecraft charging w hen ECSS-E-ST-20-07 addresses electromagnetic effects of electrostatic discharges.
Annexes A to C of ECSS-E-ST-20 document EMC activities related to ECSS-E-ST-20-07: the EMC Control Plan (Annex A) defines the approach, methods, procedures, resources, and organization, the Electromagnetic Effects Verification Plan (Annex B) defines and specifies the verification processes, analyses and tests, and the Electromagnetic Effects Verification Report (Annex C) document verification results. The EMEVP and the EMEVR are the vehicles for tailoring this standard.

  • Standard
    103 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    100 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 16603-10-03:2022(Main)
Space engineering - Testing
EN 16603-10-03:2022

This standard addresses the requirements for performing verification by testing of space segment elements and space segment equipment on ground prior to launch. The document is applicable for tests performed on qualification models, flight models (tested at acceptance level) and protoflight models.
The standard provides:
• Requirements for test programme and test management,
• Requirements for retesting,
• Requirements for redundancy testing,
• Requirements for environmental tests,
• General requirements for functional and performance tests,
NOTE Specific requirements for functional and performance tests are not part of this standard since they are defined in the specific project documentation.
• Requirements for qualification, acceptance, and protoflight testing including qualification, acceptance, and protofight models’ test margins and duration,
• Requirements for test factors, test condition, test tolerances, and test accuracies,
• General requirements for development tests pertinent to the start of the qualification test programme,
NOTE Development tests are specific and are addressed in various engineering discipline standards.
• Content of the necessary documentation for testing activities (e.g. DRD).
Due to the specific aspects of the follow ing types of test, this Standard does not address:
• Space system testing (i.e. testing above space segment element), in particular the system validation test,
• In-orbit testing,
• Testing of space segment subsystems,
NOTE Tests of space segment subsystems are often limited to functional tests that, in some case, are run on dedicated models. If relevant, qualification tests for space segment subsystems are assumed to be covered in the relevant discipline standards.
Testing of hardware below space segment equipment levels (including assembly, parts, and components),
• Testing of stand-alone software,
NOTE For verification of flight or ground softw are, EN 16603-40 (ECSS-E-ST-40) and EN 16602-80 (ECSS-Q-ST-80) apply.
• Qualification testing of tw o-phase heat transport equipment,
NOTE For qualification testing of tw o-phase heat transport equipment, EN 16603-31-02 (ECSS-E-ST-31-02) applies.
• Tests of launcher segment, subsystem and equipment, and launch facilities,
• Tests of facilities and ground support equipment,
• Tests of ground segment.
This activity will be the update of EN16603-10-03:2014
NOTE: Parallel development of update of EN Standard and the new European TR17603-10-03.

  • Standard
    132 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    127 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST-TP CEN/CLC/TR 17603-10-03:2022(Main)
Space engineering - Testing guidelines
CEN/CLC/TR 17603-10-03:2022

This handbook provides additional information for the application of the Testing standard EN 16603-10-03.
This handbook will be the guideline for all space projects, related equipment and complete systems, by providing background information that aids the reader to better understand and meet the requirements of the standard.
The document would follow the flow of the Testing standard and in particular w hatever is excluded from the testing standard (see Scope of EN 16603-10-03) should also be excluded.
NOTE: EN 16603-10-03:2014 will be in parallel also updated to take into account the new TR.

  • Technical report
    267 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    265 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 16603-50:2022(Main)
Space engineering - Communications
EN 16603-50:2022

This Standard specifies the requirements for the development of the end­to­end data communications system for spacecraft.
Specifically, this standard specifies:
-   The terminology to be used for space communication systems engineering.
-   The activities to be performed as part of the space communication system engineering process, in accordance with the ECSS-E-ST-10 standard.
-   Specific requirements on space communication systems in respect of functionality and performance.
The communications links covered by this Standard are the space­to­ground and space­to­space links used during spacecraft operations, and the communications links to the spacecraft used during the assembly, integration and test, and operational phases.
Spacecraft end­to­end communication systems comprise components in three distinct domains, namely the ground network, the space link, and the space network. This Standard covers the components of the space link and space network in detail. However, this Standard only covers those aspects of the ground network that are necessary for the provision of the end­to­end communication services.
NOTE    Other aspects of the ground network are covered in ECSS-E ST 70.
This Standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S ST 00.

  • Standard
    79 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    79 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 16603-50-25:2022(Main)
Space engineering - Adoption Notice of CCSDS 232.0-B-3, TC Space Data Link Protocol
EN 16603-50-25:2022

This document identifies the clauses and requirements modified w ith respect to the standard CCSDS 131.0-B-3, TM Synchronization and Channel Coding, Issue 3, September 2017 for application in ECSS.

  • Standard
    19 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    19 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 16603-50-26:2022(Main)
Space engineering - Adoption Notice of CCSDS 232.1-B-2, Communications Operation Procedure-1
EN 16603-50-26:2022

This document identifies the clauses and requirements modified with respect to the standards CCSDS 232.1-B-2, Communications Operation Procedure-1, Issue 2, September 2010 for application in ECSS.
NOTE The recently published technical corrigendum has modified CCSDS 232.1-B-2. However, the changes are not affecting the Adoption Notice.

  • Standard
    11 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    11 pages
    English language
    sale 10% off
    e-Library read for
    1 day