iTeh StandardsiTeh Standards
EURUSD
Your shopping cart is empty.
CEN

EN 16603-50-05:2014/AC:2017

(Corrigendum)

Space engineering - Radio frequency and modulation

Space engineering - Radio frequency and modulation

TC - Mistake in formula

Raumfahrttechnik - Funkfrequenzen und -modulation

Ingénierie spatiale - Radio fréquence et modulation

Vesoljska tehnika - Radijske frekvence in modulacija - Popravek AC

General Information

Status
Published
Publication Date
14-Mar-2017
ICS
49.140 - Space systems and operations
Technical Committee
CEN/CLC/TC 5 - Space
Drafting Committee
CEN/CLC/TC 5 - Space
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Start Date
15-Mar-2017
Due Date
15-Mar-2017
Completion Date
15-Mar-2017
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 16603-50-05:2014/AC:2017 - Space engineering - Radio frequency and modulation

Relations

Corrects
EN 16603-50-05:2014 - Space engineering - Radio frequency and modulation
Effective Date
01-Feb-2017

Buy Standard

EN 16603-50-05:2014/AC:2017EN 16603-50-05:2014/AC:2017
PreviousNext
Corrigendum
EN 16603-50-05:2014/AC:2017
English language
2 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 - Radijske frekvence in modulacija - Popravek ACRaumfahrttechnik - Funkfrequenzen und -modulationIngénierie spatiale - Radio fréquence et modulationSpace engineering - Radio frequency and modulation49.140Vesoljski sistemi in operacijeSpace systems and operations33.060.01Radijske komunikacije na splošnoRadiocommunications in generalICS:Ta slovenski standard je istoveten z:EN 16603-50-05:2014/AC:2017SIST EN 16603-50-05:2014/AC:2017en,fr,de01-maj-2017SIST EN 16603-50-05:2014/AC:2017SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16603-50-05:2014/AC
March 2017
Mars 2017
März 2017 ICS 49.140 English version Version Française Deutsche Fassung
Space engineering - Radio frequency and modulation
Ingénierie spatiale - Radio fréquence et modulation
Raumfahrttechnik - Funkfrequenzen und -modulation This corrigendum becomes effective on 15 March 2017 for incorporation in the official English version of the
...

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

CEN
EN 16605:2024(Main)
Space - Galileo Timing Receiver - Functional and Performance Requirements and associated Tests
SIST EN 16605:2025

This document is intended to stablish and define functional and performance requirements and associated tests for Galileo Timing Receivers. This document covers the following topics related to Galileo Timing Receivers:
- GNSS constellations and frequencies processed: Galileo plus additionally GPS, with nominal mode being dual-frequency processing,
- Time scales processed, including at least Galileo System Time and Universal Time Coordinate,
- User dynamics, with two operation modes: static users with well-known and static antenna position and dynamics users with moving antenna,
- Holdover devices,
- Nominal and back-up modes, including single-frequency modes, single-constellation modes and holdover mode.
- Processing of timing integrity information disseminated by the Galileo System,
- Time Receiver Autonomous Integrity Monitoring processing,
- Anti-jamming and anti-spoofing capabilities, including Automatic Gain Control monitoring and Galileo Open Service Navigation Message Authentication processing,
- Robustness to multipath.
In addition, this document gives guidelines for the installation and maintenance of the receiver, including antenna, cabling and receiver installation, initial and periodic receiver calibration, and periodic maintenance.
On top of the functional requirements, performance requirements this document defines in terms of different key performance indicators such as:
- Accuracy, availability, continuity and integrity requirements,
- T-RAIM performances, including time to alert,
- Holdover performances including maximum degradation of the timing solution with time and maximum holdover time,
This document also gives a simple test suite to verify the most fundamental requirements of the Galileo Timing Receivers.

  • Standard
    112 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 16603-20-40:2023(Main)
Space engineering - ASIC, FPGA and IP Core engineering
SIST EN 16603-20-40:2024

This activity w ill be the parallel development of EN 16603-20-40 and ECSS-E-ST-20-40C.
The scope shall cover the areas of existing ASIC and FPGA engineering chapter 5 of ECSS-Q-ST-60-02C, but w ith w ider breadth and greater depth, covering engineering requirements of end-to-end development flow s, from specification of requirements to validation of prototypes, of the follow ing monolithic devices for its use in space:
• ASICs (distinguishing digital, analogue and mixed-signal development flow s)
• FPGAs (distinguishing three technology families: SRAM, FLASH and anti-fuse technologies)
• ASIC and FPGA System-on-Chip embedding processor cores w hich have external “softw are programme” dependencies to be addressed during the SoC development, resulting in SW-HW co-design requirements.

  • Standard
    139 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 16604-10:2023(Main)
Space sustainability - Space debris mitigation requirements (ISO 24113:2023, modified)
SIST EN 16604-10:2024

This document defines the primary space debris mitigation requirements applicable to all elements of unmanned systems launched into, or passing through, near-Earth space, including launch vehicle orbital stages, operating spacecraft and any objects released as part of normal operations.

  • Standard
    20 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 16603-20:2023(Main)
Space engineering - Electrical and electronic
SIST EN 16603-20:2024

Scope remains unchanged.
This Standard establishes the basic rules and general principles applicable to the electrical, electronic, electromagnetic, microwave and engineering processes. It specifies the tasks of these engineering processes and the basic performance and design requirements in each discipline.
It defines the terminology for the activities within these areas.
It defines the specific requirements for electrical subsystems and payloads, deriving from the system engineering requirements laid out in EN 16603-10 (equivalent of ECSS-E-ST-10 "Space engineering - System engineering general requirements".)

  • Standard
    135 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 16603-20-08:2023(Main)
Space engineering - Photovoltaic assemblies and components
SIST EN 16603-20-08:2023

This Standard specifies the general requirements for the qualification, procurement, storage and delivery of photovoltaic assemblies, solar cell assemblies, bare solar cells, coverglasses and protection diodes suitable for space applications.
This standard does not cover the particular qualification requirements for a specific mission.
This Standard primarily applies to qualification approval for photovoltaic assemblies, solar cell assemblies, bare solar cells, coverglasses and protection diodes, and to the procurement of these items.
This standard is limited to crystaline Silicon and single and multi-junction GaAs solar cells with a thickness of more than 50 m and does not include thin film solar cell technologies and poly-crystaline solar cells.
This Standard does not cover the concentration technology, and especially the requirements related to the optical components of a concentrator (e.g. reflector and lens) and their verification (e.g. collimated light source).
This Standard does not apply to qualification of the solar array subsystem, solar panels, structure and solar array mechanisms.

  • Standard
    230 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 16602-60-13:2023(Main)
Space product assurance - Commercial electrical, electronic and electromechanical (EEE) components
SIST 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
CEN
EN 16602-60:2023(Main)
Space product assurance - Electrical, electronic and electromechanical (EEE) components
SIST 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
CEN
EN 16602-70-40:2023(Main)
Space product assurance - Processing and quality assurance requirements for hard brazing of metallic materials for flight hardware
SIST 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
CEN
EN 16602-70-61:2022(Main)
Space product assurance - High-reliability soldering for surface mount, mixed technology and hand-mounted electrical connections
SIST 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
CEN
EN 16603-20-07:2022(Main)
Space engineering - Electromagnetic compatibility
SIST 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