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CEN/CLC/TR 17603-31-16:2021

(Main)

Space Engineering - Thermal design handbook - Part 16: Thermal Protection System

Space Engineering - Thermal design handbook - Part 16: Thermal Protection System

The thermal protection system (TPS) of a space vehicle ensures the structural integrity of the surface of the craft and maintains the correct internal temperatures (for crew, electronic equipment, etc.) when the vehicle is under the severe thermal loads of re-entry. These loads are characterised by very large heat fluxes over the relatively short period of re-entry.
The design of thermal protection systems for re-entry vehicles is very complex due to the number and complexity of phenomena involved: the flow around the vehicle is hypersonic, tridimensional and reactive, and its interaction with the vehicle’s surface may induce chemical reactions which are not fully understood.
Two TPS concepts for re-entry vehicles, ablative and radiative are examined and there is also an anlyisis of existing systems using them.
The Thermal design handbook is published in 16 Parts
TR 17603-31-01 Part 1A    Thermal design handbook – Part 1: View factors
TR 17603-31-01 Part 2A    Thermal design handbook – Part 2: Holes, Grooves and Cavities
TR 17603-31-01 Part 3A    Thermal design handbook – Part 3: Spacecraft Surface Temperature
TR 17603-31-01 Part 4A    Thermal design handbook – Part 4: Conductive Heat Transfer
TR 17603-31-01 Part 5A    Thermal design handbook – Part 5: Structural Materials: Metallic and Composite
TR 17603-31-01 Part 6A    Thermal design handbook – Part 6: Thermal Control Surfaces
TR 17603-31-01 Part 7A    Thermal design handbook – Part 7: Insulations
TR 17603-31-01 Part 8A    Thermal design handbook – Part 8: Heat Pipes
TR 17603-31-01 Part 9A    Thermal design handbook – Part 9: Radiators
TR 17603-31-01 Part 10A    Thermal design handbook – Part 10: Phase – Change Capacitors
TR 17603-31-01 Part 11A    Thermal design handbook – Part 11: Electrical Heating
TR 17603-31-01 Part 12A    Thermal design handbook – Part 12: Louvers
TR 17603-31-01 Part 13A    Thermal design handbook – Part 13: Fluid Loops
TR 17603-31-01 Part 14A    Thermal design handbook – Part 14: Cryogenic Cooling
TR 17603-31-01 Part 15A    Thermal design handbook – Part 15: Existing Satellites
TR 17603-31-01 Part 16A    Thermal design handbook – Part 16: Thermal Protection System

Raumfahrttechnik - Handbuch für thermisches Design - Teil 16: Thermalschutzsysteme

Ingénierie spatiale - Manuel de conception thermique - Partie 16 : Protection Thermique des véhicules spatiaux

Vesoljska tehnika - Priročnik o toplotni zasnovi - 16. del: Sistem toplotne zaščite

General Information

Status
Published
Publication Date
10-Aug-2021
ICS
49.140 - Space systems and operations
Technical Committee
CEN/CLC/TC 5 - Space
Drafting Committee
CEN/CLC/TC 5/WG 6 - Upstream standards
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Start Date
11-Aug-2021
Due Date
14-Jul-2022
Completion Date
11-Aug-2021
Mandate
M/496 - Mandate addressed to CEN, CENELEC and ETSI to develop standardisation regarding space industry (Phase 3 of the process)
Ref Project
SIST-TP CEN/CLC/TR 17603-31-16:2021 - Space Engineering - Thermal design handbook - Part 16: Thermal Protection System

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Standards Content (Sample)

SLOVENSKI STANDARD
SIST-TP CEN/CLC/TR 17603-31-16:2021
01-oktober-2021
Vesoljska tehnika - Priročnik o toplotni zasnovi - 16. del: Sistem toplotne zaščite
Space Engineering - Thermal design handbook - Part 16: Thermal Protection System
Raumfahrttechnik - Handbuch für thermisches Design - Teil 16: Wärmeschutzsystem
Ingénierie spatiale - Manuel de conception thermique - Partie 16: Protection Thermique
des véhicules spatiaux
Ta slovenski standard je istoveten z: CEN/CLC/TR 17603-31-16:2021
ICS:
49.140 Vesoljski sistemi in operacije Space systems and
operations
SIST-TP CEN/CLC/TR 17603-31-16:2021 en,fr,de
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST-TP CEN/CLC/TR 17603-31-16:2021

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SIST-TP CEN/CLC/TR 17603-31-16:2021


TECHNICAL REPORT
CEN/CLC/TR 17603-31-
16
RAPPORT TECHNIQUE

TECHNISCHER BERICHT

August 2021
ICS 49.140

English version

Space Engineering - Thermal design handbook - Part 16:
Thermal Protection System
Ingénierie spatiale - Manuel de conception thermique - Raumfahrttechnik - Handbuch für thermisches Design -
Partie 16 : Protection Thermique des véhicules Teil 16: Thermalschutzsysteme
spatiaux


This Technical Report was approved by CEN on 28 June 2021. It has been drawn up by the Technical Committee CEN/CLC/JTC 5.

CEN and CENELEC members are the national standards bodies and national electrotechnical committees of Austria, Belgium,
Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy,
Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Republic of North Macedonia, Romania, Serbia,
Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom.
























CEN-CENELEC Management Centre:
Rue de la Science 23, B-1040 Brussels
© 2021 CEN/CENELEC All rights of exploitation in any form and by any means Ref. No. CEN/CLC/TR 17603-31-16:2021 E
reserved worldwide for CEN national Members and for
CENELEC Members.

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SIST-TP CEN/CLC/TR 17603-31-16:2021
CEN/CLC/TR 17603-31-16:2021 (E)
Table of contents
European Foreword . 5
1 Scope . 6
2 References . 7
3 Terms, definitions and symbols . 8
3.1 Terms and definitions . 8
3.2 Abbreviated terms. 8
4 Introduction . 9
4.1 General .9
4.2 Classification of thermal protection systems . 10
5 Ablative systems . 14
5.1 General . 14
5.2 Ablative materials . 14
5.3 Basic analysis . 15
5.3.1 Surface equilibrium . 16
5.4 Existing systems . 19
5.4.1 Galileo probe . 19
6 Radiative systems . 23
6.1 General . 23
6.2 Radiative materials . 23
6.3 Existing systems . 24
6.3.1 Space shuttle . 24
6.4 Other developments .
...

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