iTeh StandardsiTeh Standards
EURUSD
Your shopping cart is empty.
SIST

SIST EN 14824:2004

(Main)

Space engineering - Testing

Space engineering - Testing

This European Standard,
a) specifies standard environmental and performance test requirements for a space system and its constituents;
b) specifies the test requirements for products and systems that are generally applicable to all projects;
c) specifies the documentation associated with testing activities;
d) is applicable to all types and combinations of project, organization and product;
e) is applicable to space systems and its constituents; and
f) covers each stage of verification by testing, for a space system from development to post-landing.
This European Standard does not specify acceptance criteria, specifications or procedures for any particular project or class of projects. In addition this Standard does not apply to software testing, hardware below equipment levels, nor covers the following:

Raumfahrttechnik - Tests

Space engineering - Testing

General Information

Status
Withdrawn
Publication Date
30-Apr-2004
Withdrawal Date
20-Oct-2014
ICS
49.140 - Space systems and operations
Technical Committee
I08 - Imaginarni 08
Current Stage
9900 - Withdrawal (Adopted Project)
Start Date
16-Oct-2014
Due Date
08-Nov-2014
Completion Date
21-Oct-2014
Mandate
M/237 - Mandate to CEN, CENELEC and ETSI for standardization in the field of equipment for the space industry
Ref Project
EN 14824:2003 - Space engineering - Testing

Relations

Replaced By
SIST EN 16603-10-03:2014 - Space engineering - Testing
Effective Date
01-Nov-2014

Buy Standard

EN 14824:2004EN 14824:2004
PreviousNext
Standard
EN 14824:2004
English language
143 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.Space engineering - TestingRaumfahrttechnik - TestsSpace engineering - Testing49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 14824:2003SIST EN 14824:2004en01-maj-2004SIST EN 14824:2004SLOVENSKI
STANDARD



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN 14824:2004



SIST EN
...

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 14736:2004(Main)
Space product assurance - Quality assurance for test centres
EN 14736:2004

This European Standard defines the quality assurance (QA) requirements for the operation, maintenance, management and configuration control of test centres for space applications. It also defines the requirements for the treatment of test specimens and the development of test facilities.
This European Standard applies to test centres as self-standing organizations, or those belonging to a parent organization. Separate procedures are not required in the latter case if activities are controlled by the implementation of parent organization procedures.
When viewed in a specific project context, the requirements defined in this European Standard should be tailored to match the genuine requirements of a particular profile and circumstances of a project.

  • Standard
    31 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN ISO 16091:2004(Main)
Space systems - Integrated logistic support (ISO 16091:2002)
EN ISO 16091:2002

The present document, "Integrated Logistic Support", is part of a collection of space standards belonging to the management branch. This standard describes the set of management requirements aimed at the identification and provision of logistical support, such that the consumer can operate and maintain a product in its operational conditions, for the expected lifetime.

  • Standard
    27 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 14724:2004(Main)
Space project management - Tailoring of space standards
EN 14724:2003

This Standard is part of a collection of European Space Standards dealing with management. It defines the process of tailoring, applicable to all space standards for management, product assurance and engineering as a guideline. This Standard defines the objectives, principles, methods and processes of tailoring, which are necessary for the establishment of project requirement documents.

  • Standard
    18 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 13291-3:2004(Main)
Space product assurance - General requirements - Part 3: Materials, mechanical parts and processes
EN 13291-3:2003

The purpose of this standard is to define the requirements and statements applicable to materials, mechanical parts and processes to satisfy the mission performance requirements. This standard covers the following requirement domains: - management, including organisation, reviews, acceptance status and documentation control; - selection criteria and rules; - evaluation, validation/qualification testing; - procurement and receiving inspection; - utilisation criteria and rules. The relationship between activities and programme phases is defined in annex A.

  • Standard
    22 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN ISO 14620-1:2004(Main)
Space systems - Safety requirements - Part 1: System safety (ISO 14620-1:2002)
EN ISO 14620-1:2002

This standard defines the safety programme and the technical safety requirements that shall be implemented in order to comply with the ECSS Safety Policy as defined in ECSS-Q-00. It is intended to protect flight and ground personnel, the launch vehicle, associated payloads, ground support equipment, the general public, public and private property, and the environment from hazards associated with European space systems.

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