Space Engineering - Thermal design handbook - Part 5: Structural Materials: Metallic and Composite

In this Part 5 of the spacecraft thermal control and design data handbooks, clause 4 contains technical data on the metallic alloys used in spacecrafts is given: composition, application areas, properties and behaviour from a thermal and thermo-optics point of view, degeneration and aging. All other properties of the metallic alloys are outside the scope of this document.
Properties of composite materials combined to form heterogeneous structures are given in clause 5.
The Thermal design handbook is published in 16 Parts
TR 17603-31-01 Part 1
Thermal design handbook – Part 1: View factors
TR 17603-31-01 Part 2
Thermal design handbook – Part 2: Holes, Grooves and Cavities
TR 17603-31-01 Part 3
Thermal design handbook – Part 3: Spacecraft Surface Temperature
TR 17603-31-01 Part 4
Thermal design handbook – Part 4: Conductive Heat Transfer
TR 17603-31-01 Part 5
Thermal design handbook – Part 5: Structural Materials: Metallic and Composite
TR 17603-31-01 Part 6
Thermal design handbook – Part 6: Thermal Control Surfaces
TR 17603-31-01 Part 7
Thermal design handbook – Part 7: Insulations
TR 17603-31-01 Part 8
Thermal design handbook – Part 8: Heat Pipes
TR 17603-31-01 Part 9
Thermal design handbook – Part 9: Radiators
TR 17603-31-01 Part 10
Thermal design handbook – Part 10: Phase – Change Capacitors
TR 17603-31-01 Part 11
Thermal design handbook – Part 11: Electrical Heating
TR 17603-31-01 Part 12
Thermal design handbook – Part 12: Louvers
TR 17603-31-01 Part 13
Thermal design handbook – Part 13: Fluid Loops
TR 17603-31-01 Part 14
Thermal design handbook – Part 14: Cryogenic Cooling
TR 17603-31-01 Part 15
Thermal design handbook – Part 15: Existing Satellites
TR 17603-31-01 Part 16
Thermal design handbook – Part 16: Thermal Protection System

Raumfahrttechnik - Handbuch für thermisches Design - Teil 5: Konstruktionswerkstoffe: Metallisch und Verbundwerkstoffe

Ingénierie spatiale - Manuel de conception thermique - Partie 5: Matériaux structuraux: métalliques et composites

Vesoljska tehnika - Priročnik o toplotni zasnovi - 5. del: Strukturni materiali: kovinski in kompozitni

General Information

Status
Published
Public Enquiry End Date
12-May-2021
Publication Date
19-Aug-2021
Technical Committee
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
16-Aug-2021
Due Date
21-Oct-2021
Completion Date
20-Aug-2021

Buy Standard

Technical report
TP CEN/CLC/TR 17603-31-05:2021
English language
398 pages
sale 10% off
Preview
sale 10% off
Preview
e-Library read for
1 day
Draft
kTP FprCEN/CLC/TR 17603-31-05:2021
English language
398 pages
sale 10% off
Preview
sale 10% off
Preview
e-Library read for
1 day

Standards Content (Sample)

SLOVENSKI STANDARD
SIST-TP CEN/CLC/TR 17603-31-05:2021
01-oktober-2021
Vesoljska tehnika - Priročnik o toplotni zasnovi - 5. del: Strukturni materiali:
kovinski in kompozitni
Space Engineering - Thermal design handbook - Part 5: Structural Materials: Metallic
and Composite
Raumfahrttechnik - Handbuch für thermisches Design - Teil 5: Konstruktionswerkstoffe:
Metallisch und Verbundwerkstoffe
Ingénierie spatiale - Manuel de conception thermique - Partie 5: Matériaux structuraux:
métalliques et composites
Ta slovenski standard je istoveten z: CEN/CLC/TR 17603-31-05:2021
ICS:
49.140 Vesoljski sistemi in operacije Space systems and
operations
SIST-TP CEN/CLC/TR 17603-31-05:2021 en,fr,de
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

---------------------- Page: 1 ----------------------
SIST-TP CEN/CLC/TR 17603-31-05:2021

---------------------- Page: 2 ----------------------
SIST-TP CEN/CLC/TR 17603-31-05:2021


TECHNICAL REPORT
CEN/CLC/TR 17603-31-
05
RAPPORT TECHNIQUE

TECHNISCHER BERICHT

August 2021
ICS 49.140

English version

Space Engineering - Thermal design handbook - Part 5:
Structural Materials: Metallic and Composite
Ingénierie spatiale - Manuel de conception thermique - Raumfahrttechnik - Handbuch für thermisches Design -
Partie 5 : Matériaux de structure : métalliques et Teil 5: Strukturmaterialien: Metalle und Verbundstoffe
composites


This Technical Report was approved by CEN on 14 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 17603-31-05:2021 E
reserved worldwide for CEN national Members and for
CENELEC Members.

---------------------- Page: 3 ----------------------
SIST-TP CEN/CLC/TR 17603-31-05:2021
CEN/CLC/TR 17603-31-05:2021 (E)
Table of contents
European Foreword . 17
1 Scope . 18
2 References . 19
3 Terms, definitions and symbols . 20
3.1 Terms and definitions . 20
3.2 Symbols . 20
4 Metallic materials . 23
4.1 General . 23
4.1.1 Modifiers of thermal radiative properties . 26
4.1.2 Cladding definitions . 27
4.1.3 Temper designation for heat treatable aluminium alloys . 28
4.2 Aluminium alloys . 28
4.3 Aluminium-Copper alloys . 85
4.4 Aluminium-Magnesium alloys . 104
4.5 Aluminium-Zinc alloys . 114
4.6 Magnesium-Zink-Thorium alloys . 131
4.7 Titanium-Aluminium-Tin alloys . 133
4.8 Titanium-Aluminium-Tin alloys . 144
4.9 Titanium-Aluminium-Vanadium alloys . 151
4.10 Nickel-Chrome-Cobalt-Molybdenum alloys . 165
4.11 Iron-Nickel alloys . 175
5 Composite materials . 182
5.1 List of symbols . 182
5.2 List of matrices, prepregs and laminates quoted in this clause . 187
5.2.1 Matrices, adhesives, potting, moulding compounds . 188
5.2.2 Prepregs, laminates and films . 193
5.2.3 Code list of manufacturers (or developers) . 195
5.3 General introduction . 197
5.3.2 Composition . 198
2

---------------------- Page: 4 ----------------------
SIST-TP CEN/CLC/TR 17603-31-05:2021
CEN/CLC/TR 17603-31-05:2021 (E)
5.3.3 Commercial fiber product names, descriptions and manufacturers . 200
5.3.4 Geometry of fiber reinforcement. fabrics. abridged designation . 205
5.4 Physical properties . 210
5.4.1 Density . 210
5.5 Thermal properties . 216
5.5.1 Specific heat . 216
5.5.2 Thermal conductivity . 222
5.5.3 Thermal diffusivity . 247
5.6 Thermo-elastic properties . 256
5.6.1 Coefficient of linear thermal expansion . 256
5.7 Thermal radiation properties of bare high strength fibers . 319
5.7.1 Sample characterization . 319
5.7.2 Emittance . 319
5.7.3 Absorptance . 321
5.8 Thermal radiation properties of bare composite materials . 324
5.8.1 Tabulated data . 324
5.9 Thermal radiation properties of coated composite materials . 326
5.9.1 White painted composite materials . 327
5.9.2 Sputtered Aluminium on graphite-epoxy composite material . 331
5.10 Operating temperature range . 334
5.10.1 Temperatures related to the maximum service temperature . 335
5.11 Electrical properties . 341
5.11.1 Electrical resistance and electrical resistivity . 341
5.12 Prelaunch environmental effects . 348
5.12.1 Moisture absorption and desorption . 348
5.13 Postlaunch environmental effects . 355
5.13.1 Ascent . 355
5.13.2 Orbital effects . 357
5.13.3 Re-entry effects . 367
5.14 Thermal vacuum cycling . 371
5.14.1 Test facilities . 371
5.14.2 Measurement methods . 372
5.14.3 Thermal vacuum cycling effects on the coefficient of linear thermal
expansion . 373
5.14.4 Trends in the variation of mechanical properties . 378
5.15 Coating application . 378
5.15.1 Pcbz conductive white paint . 378
5.15.2 APA-2474 (TiO white paint) . 378
2
3

---------------------- Page: 5 ----------------------
SIST-TP CEN/CLC/TR 17603-31-05:2021
CEN/CLC/TR 17603-31-05:2021 (E)
5.15.3 Wiederhold's Z-12321 . 379
5.16 Past spatial uses . 380
5.16.1 Intelsat v . 380
5.16.2 Spelda (structure porteuse externe de lancement double ariane) . 381
5.16.3 CS-3A Japanese satellite . 384
Bibliography metalic materials . 387
References composite materials . 391

Figures
Figure 4-1: Specific heat, c, of Aluminium as a function of temperature, T. 30
Figure 4-2: Thermal conductivity, κ, of Aluminium as a function of temperature, T. . 31
Figure 4-3: Thermal conductivity integrals of Aluminium as a function of temperature, Τ. . 32
Figure 4-4: Thermal diffusivity, α , of Aluminium as a function of temperature, Τ . . 33
Figure 4-5: Linear thermal expansion, ∆L / L, of Aluminium as a function of
temperature, Τ. 34
Figure 4-6: Normal spectral emittance, ε ', of Aluminium as a function of wavelength, λ. . 37
λ
Figure 4-7: Normal spectral emittance, ε ', of Aluminium conversion coatings as a
λ
function of wavelength, λ. . 38
Figure 4-8: Angular spectral emittance, ε ', of Aluminium as a function of wavelength, λ. . 39
λ
Figure 4-9: Normal total emittance, ε', of Aluminium as a function of temperature, Τ. . 45
Figure 4-10: Normal total emittance, ε', of Aluminium anodized as a function of
anodizing thickness, t . . 46
c
Figure 4-11: Summary of data concerning the hemispherical total emittance, ε , of
Aluminium as a function of temperature, Τ. From Touloukian & DeWitt
(1970) [42]. . 47
Figure 4-12: Summary of data concerning the hemispherical total emittance, ε , of
Aluminium conversion coatings vs. temperature, Τ. From Touloukian,
DeWitt & Hernicz (1972) [43]. . 52
Figure 4-13: Directional spectral absorptance, α ', of Aluminium as a function of
λ
wavelength, λ. Data points correspond to β = 25°. . 54
Figure 4-14: Absorptance to emittance ratio, α /ε , of Aluminium conversion coatings as
s
a function of the exposure time, t. . 60
Figure 4-15: Normal - normal spectral reflectance, ρ '', of Aluminium as a function of
λ
wavelength, λ. . 62
Figure 4-16: Normal - normal spectral reflectance, ρ '', of Aluminium contact coatings
λ
as a function of wavelength, λ. . 64
Figure 4-17: Effect of coating thickness on normal - normal spectral reflectance, ρ '', of
λ
Aluminium conversion coatings as a function of wavelength, λ. . 65
Figure 4-18: Bidirectional reflectance, ρ '', of Aluminium contact coatings as a function
λ
of wavelength, λ. . 66
4

---------------------- Page: 6 ----------------------
SIST-TP CEN/CLC/TR 17603-31-05:2021
CEN/CLC/TR 17603-31-05:2021 (E)
Figure 4-19: Bidirectional spectral reflectance, ρλ'', of Aluminium conversion coatings
as a function of zenith angles, β and β ', of incident and reflected radiations. . 68
Figure 4-20: Summary of data concerning normal - hemispherical spectral reflectance,
ρ ', of Aluminium vs. wavelength, λ. From Touloukian & DeWitt (1970) [42]. . 69
λ
Figure 4-21: Normal - hemispherical spectral reflectance, ρ ', of Aluminium conversion
λ
coatings as a function of wavelength, λ. . 70
Figure 4-22: Effect of UV exposure on normal - hemispherical spectral reflectance, ρ ',
λ
of Aluminium conversion coatings as a function of wavelength, λ. 71
Figure 4-23: Effect of electron exposure on normal - hemispherical spectral reflectance
of Aluminium conversion coatings as a function of wavelength, λ. 72
Figure 4-24: Effect of simultaneous UV - electron exposure on normal - hemispherical
spectral reflectance, ρ ', of Aluminium conversion coatings as a function of
λ
wavelength, λ. . 73
Figure 4-25: Effect of proton exposure on normal - hemispherical spectral
reflectance, ρ' , of Aluminium conversion coatings as a function of
λ
wavelength, λ. . 74
Figure 4-26: Directional - hemispherical spectral reflectance, ρ ', of Aluminium
λ
conversion coatings as a function of wavelength, λ. . 75
Figure 4-27: Hemispherical - normal spectral reflectance, ρ ', of Aluminium contact
λ
coatings as a function of wavelength, λ. . 76
Figure 4-28: Bidirectional total reflectance, ρ'', of Aluminium as a function of the viewing
zenith angles, β'. . 77
Figure 4-29: Normal - normal spectral transmittance, τ '', of Aluminium as a function of
λ
wavelength, λ. . 80
Figure 4-30: Angular spectral transmittance, τ '', of Aluminium as a function of
λ
wavelength, λ. . 81
−1
Figure 4-31: Electrical resistivity, σ , of Aluminium as a function of temperature, Τ. . 83
Figure 4-32: Specific heat, c, of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a function of
temperature, Τ. 86
Figure 4-33: Thermal conductivity, k, of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a function of
temperature, Τ. 87
Figure 4-34: Thermal conductivity integrals of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a
function of temperature, Τ. . 88
α, of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a function of
Figure 4-35: Thermal diffusivity,
temperature, Τ. 89
Figure 4-36: Linear thermal expansion, ∆L / L, of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a
function of temperature, Τ. . 90
Figure 4-37: Normal - spectral emittance, ε ', of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a
λ
function of wavelength, λ. . 91
Figure 4-38: Normal total emittance, ε', of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a function of
temperature, T. 93
Figure 4-39: Normal-normal spectral reflectance, ρ '', of Al-4,3 Cu-1,5 Mg-0,6 Mn,
λ
anodized, as a function of wavelength, λ. . 98
5

---------------------- Page: 7 ----------------------
SIST-TP CEN/CLC/TR 17603-31-05:2021
CEN/CLC/TR 17603-31-05:2021 (E)
Figure 4-40: Normal - hemispherical spectral reflectance, ρλ', of Al - 4,3 Cu - 1,5 Mg -
0,6 Mn as a function of wavelength, λ. . 99
Figure 4-41: Normal - hemispherical spectral reflectance, ρ ', of Al - 4,3 Cu - 1,5 Mg -
λ
0,6 Mn, anodized, as a function of wavelength, λ. . 100
Figure 4-42: Normal-hemispherical spectral reflectance, ρ ', of Al-1 Mg-0,6 Si, as
λ
received, as a function of wavelength, λ. . 108
Figure 4-43: Normal-hemispherical spectral reflectance, ρ ', of Al-1 Mg-0,6 Si, grit
λ
blasted, as a function of wavelength, λ. . 109
Figure 4-44: Normal-hemispherical spectral reflectance, ρ ', of Al-1 Mg-0,6 Si,
λ
chemically polished, as a function of wavelength, λ. . 111
Figure 4-45: Normal - hemispherical spectral reflectance, ρ ', of Al - 1 Mg - 0,6 Si,
λ
chemically milled, as a function of wavelength, λ. . 112
Figure 4-46: Specific heat, c, of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a function of
temperature, Τ. 115
Figure 4-47: Thermal conductivity, k, of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a function of
temperature, T. 116
Figure 4-48: Thermal conductivity integral of Al – 5,7 Zn – 2,5 Mg – 1,6 Cu as a
function of temperature, T. . 117
Figure 4-49: Thermal diffusivity, α, of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a function of
temperature, T. 118
Figure 4-50: Linear thermal expansion, ∆L / L, of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a
function of temperature, Τ. . 119
Figure 4-51: Normal spectral emittance, ε ', of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a
λ
function of wavelength, λ. . 120
Figure 4-52: Angular spectral emittance, ε ', of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a
λ
function of wavelength, λ. . 121
Figure 4-53: Normal total emittance, ε', of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a function of
temperature,Τ. 122
Figure 4-54: Normal-hemispherical spectral reflectance, ρ' , of Al - 5,7 Zn - 2,5 Mg - 1,6
λ
Cu conversion coatings, as a function of wavelngth, λ. . 126
Figure 4-55: Specific heat, c, of Ti - 5 Al - 2,5 Sn as a function of temperature, T. . 134
Figure 4-56: Thermal conductivity, k, of Ti - 5 Al - 2,5 Sn as a function of temperature,
T. 135
Figure 4-57: Thermal linear expansion, ∆L/L, of Ti - 5 Al - 2,5 Sn as a function of
temperature, T. 136
Figure 4-58: Normal spectral emittance, ελ', of Ti - 5 Al - 2,5 Sn as a function of
−7
temperature, T, for λ =6,65 x 10 m. . 137
Figure 4-59: Normal total emittance, ε', of Ti - 5 Al - 2,5 Sn as a function of
temperature, T. 138
Figure 4-60: Normal-normal spectral reflectance, ρ '', of Ti - 5 Al - 2,5 Sn as a function
λ
of wavelength, λ. . 140
Figure 4-61: Normal - hemispherical spectral reflectance, ρ ', of Ti - 5 Al - 2,5 Sn as a
λ
function of wavelength, λ. . 141
6

---------------------- Page: 8 ----------------------
SIST-TP CEN/CLC/TR 17603-31-05:2021
CEN/CLC/TR 17603-31-05:2021 (E)
Figure 4-62: Normal - hemispherical spectral reflectance, ρλ', of Ti - 5 Al - 2,5 Sn,
anodized, as a function of wavelength, λ. . 142
−1
Figure 4-63: Electrical resistivity, σ , of Ti - 5 Al - 2,5 Sn as a function of temperature,
T. 143
Figure 4-64: Specific heat, c, of Ti - 6 Al - 2 Sn - 4 Zr - 2 Mo as a function of
temperature, T. 145
Figure 4-65: Thermal conductivity, k, of Ti - 6 Al - 2 Sn - 4 Zr - 2 Mo as a function of
temperature, T. 146
Figure 4-66: Mean coefficient of linear thermal expansion, β, of Ti - 6 Al - 2 Sn - 4 Zr - 2
Mo from room temperature to temperature T. . 147
−1
Figure 4-67: Electrical resistivity, σ , of Ti - 6 Al - 2 Sn - 4 Zr - 2 Mo as a function of
temperature, T. 149
Figure 4-68: Specific heat, c, of Ti - 6 Al - 4 V as a function of temperature, T. . 152
Figure 4-69: Thermal conductivity, k, of Ti - 6 Al - 4 V as a function of temperature, T. . 153
Figure 4-70: Thermal conductivity integrals of Ti - 6 Al - 4 V as a function of
temperature, T. 154
Figure 4-71: Thermal diffusivity, α, of Ti - 6 Al - 4 V as a function of temperature, T. . 155
∆L/L, of Ti - 6 Al - 4 V as a function of
Figure 4-72: Thermal linear expansion,
temperature, T. 156
Figure 4-73: Normal spectral emittance, ε ', of Ti - 6 Al - 4 V as a function of
λ
temperature, T. 157
Figure 4-74: Normal total emittance, ε', of Ti - 6 Al - 4 V as a function of temperature, T. . 158
Figure 4-75: Hemispherical total emittance, ε, of Ti - 6 Al - 4 V as a function of
temperature, T. 160
Figure 4-76: Normal - hemispherical spectral reflectance, ρ ', of Ti - 6 Al - 4 V as a
λ
function of wavelength, λ. . 162
−1
Figure 4-77: Electrical resistivity, σ , of Ti - 6 Al - 4 V as a function of temperature, T. . 163
Figure 4-78: Specific heat, c, of Ni - 19 Cr - 11 Co - 10 Mo - 3 Ti as a function of
temperature, T. 166
Figure 4-79: Thermal conductivity, k, of Ni - 19 Cr - 11 Co - 10 Mo - 3 Ti as a function
of temperature, T. . 167
Figure 4-80: Thermal linear expansion, ∆L/L, of Ni - 19 Cr - 11 Co - 10 Mo - 3 Ti as a
function of temperature, T. . 168
Figure 4-81: Normal spectral emittance, ελ', of Ni - 19 Cr - 11 Co - 10 Mo - 3 Ti as a
function of wavelength, λ. . 169
Figure 4-82: Normal total emittance, ε', of Ni - 19 Cr - 11 Co - 10 Mo - 3 Ti as a function
of temperature, T. . 170
Figure 4-83: Normal-normal spectral reflectance, ρ" , of Ni - 19 Cr - 11 Co - 10 Mo - 3
λ
Ti as a function of wavelength, λ. Data points correspond to normal-
hemispherical reflectance while , , correspond to hemispherical-normal
reflectance. . 172
Figure 4-84: Specific heat, c, of Fe - 36 Ni (Invar) as a function of temperature, T. . 176
7

---------------------- Page: 9 ----------------------
SIST-TP CEN/CLC/TR 17603-31-05:2021
CEN/CLC/TR 17603-31-05:2021 (E)
Figure 4-85: Linear thermal expansion, ∆L/L, of Fe - 36 Ni (Invar) as a function of
temperature, T. 177
Figure 4-86: Effect of the concentration of alloying elements, c, on the value of the
coefficient of linear expansion, β. From MOND NICKEL Co. . 178
−7
Figure 4-87: Normal emittance, ε ', of Fe - 36 Ni (Invar), for λ = 6,7 x 10 as a function
λ
of temperature, T. . 179
Figure 5-1: International ties between Carbon Fiber manufactures. From SENER
(1984) [147]. . 205
Figure 5-2: Schematic of an angle plied laminate. From Chamis (1987) [67]. . 206
Figure 5-3: Schematic of a tri-orthogonally fiber reinforced composite. a) Straight
filaments. From Domínguez (1987) [82]. b) Tapes. From Aboudi (1984)
[49]. . 206
Figure 5-4: Main types of woven fabrics. Lengthwise (warp) yarns and crosswise (fill)
yarns can be interlaced to produce woven fabrics. A fabric construction of
16 x 14 means 16 warp ends per inch and 14 fill ends per inch. a) Plain
weave. Very stable. Small yarn slippage. b) Leno weave. Minimizes
distortion with few yarns. c) Twill. The fabric has a broken diagonal line
and, consequently, greater pliability than a plain weave. d) Crowfoot satin.
Pliable and confortable to contoured surfaces. From Domínguez (1987)
[82], Weeton, Peters & Thomas (1987) [164]. . 207
Figure 5-5: Longitudinal (to fibers) and transverse directions for the measurement of
composite properties. From Chamis (1987) [67]. . 209
Figure 5-6: Cryostat assemblies for measuring the thermal conductivity, k. a) High-k
samples. b) Low-k samples. From Pilling, Yates, Black & Tattersall (1979)
[137]. For explanation see text. . 222
Figure 5-7: Facility used to measure the thermal conductivity, k, of a sample as a
function of temperature in the range 90 K to 410 K. Temperature changes
continuously. From Ott (1981) [132]. . 224
Figure 5-8: Hypodermic probe to measure the the
...

SLOVENSKI STANDARD
kSIST-TP FprCEN/CLC/TR 17603-31-05:2021
01-maj-2021
Vesoljska tehnika - Priročnik za toplotno zasnovo - 5. del: Strukturni materiali:
kovinski in kompozitni
Space Engineering - Thermal design handbook - Part 5: Structural Materials: Metallic
and Composite
Raumfahrttechnik - Handbuch für thermisches Design - Teil 5: Konstruktionswerkstoffe:
Metallisch und Verbundwerkstoffe
Ingénierie spatiale - Manuel de conception thermique - Partie 5: Matériaux structuraux:
métalliques et composites
Ta slovenski standard je istoveten z: FprCEN/CLC/TR 17603-31-05
ICS:
49.140 Vesoljski sistemi in operacije Space systems and
operations
kSIST-TP FprCEN/CLC/TR 17603-31- en,fr,de
05:2021
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

---------------------- Page: 1 ----------------------
kSIST-TP FprCEN/CLC/TR 17603-31-05:2021

---------------------- Page: 2 ----------------------
kSIST-TP FprCEN/CLC/TR 17603-31-05:2021


TECHNICAL REPORT
FINAL DRAFT
FprCEN/CLC/TR 17603-
RAPPORT TECHNIQUE
31-05
TECHNISCHER BERICHT


February 2021
ICS 49.140

English version

Space Engineering - Thermal design handbook - Part 5:
Structural Materials: Metallic and Composite
Ingénierie spatiale - Manuel de conception thermique - Raumfahrttechnik - Handbuch für thermisches Design -
Partie 5: Matériaux structuraux: métalliques et Teil 5: Konstruktionswerkstoffe: Metallisch und
composites Verbundwerkstoffe


This draft Technical Report is submitted to CEN members for Vote. 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.

Recipients of this draft are invited to submit, with their comments, notification of any relevant patent rights of which they are
aware and to provide supporting documentation.

Warning : This document is not a Technical Report. It is distributed for review and comments. It is subject to change without
notice and shall not be referred to as a Technical Report.



















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. FprCEN/CLC/TR 17603-31-05:2021 E
reserved worldwide for CEN national Members and for
CENELEC Members.

---------------------- Page: 3 ----------------------
kSIST-TP FprCEN/CLC/TR 17603-31-05:2021
FprCEN/CLC/TR 17603-31-05:2021 (E)
Table of contents
European Foreword . 17
1 Scope . 18
2 References . 19
3 Terms, definitions and symbols . 20
3.1 Terms and definitions . 20
3.2 Symbols . 20
4 Metallic materials . 23
4.1 General . 23
4.1.1 Modifiers of thermal radiative properties . 26
4.1.2 Cladding definitions . 27
4.1.3 Temper designation for heat treatable aluminium alloys . 28
4.2 Aluminium alloys . 28
4.3 Aluminium-Copper alloys . 85
4.4 Aluminium-Magnesium alloys . 104
4.5 Aluminium-Zinc alloys . 114
4.6 Magnesium-Zink-Thorium alloys . 131
4.7 Titanium-Aluminium-Tin alloys . 133
4.8 Titanium-Aluminium-Tin alloys . 144
4.9 Titanium-Aluminium-Vanadium alloys . 151
4.10 Nickel-Chrome-Cobalt-Molybdenum alloys . 165
4.11 Iron-Nickel alloys . 175
5 Composite materials . 182
5.1 List of symbols . 182
5.2 List of matrices, prepregs and laminates quoted in this clause . 187
5.2.1 Matrices, adhesives, potting, moulding compounds . 188
5.2.2 Prepregs, laminates and films . 193
5.2.3 Code list of manufacturers (or developers) . 195
5.3 General introduction . 197
5.3.2 Composition . 198
2

---------------------- Page: 4 ----------------------
kSIST-TP FprCEN/CLC/TR 17603-31-05:2021
FprCEN/CLC/TR 17603-31-05:2021 (E)
5.3.3 Commercial fiber product names, descriptions and manufacturers . 200
5.3.4 Geometry of fiber reinforcement. fabrics. abridged designation . 205
5.4 Physical properties . 210
5.4.1 Density . 210
5.5 Thermal properties . 216
5.5.1 Specific heat . 216
5.5.2 Thermal conductivity . 222
5.5.3 Thermal diffusivity . 247
5.6 Thermo-elastic properties . 256
5.6.1 Coefficient of linear thermal expansion . 256
5.7 Thermal radiation properties of bare high strength fibers . 319
5.7.1 Sample characterization . 319
5.7.2 Emittance . 319
5.7.3 Absorptance . 321
5.8 Thermal radiation properties of bare composite materials . 324
5.8.1 Tabulated data . 324
5.9 Thermal radiation properties of coated composite materials . 326
5.9.1 White painted composite materials . 327
5.9.2 Sputtered Aluminium on graphite-epoxy composite material . 331
5.10 Operating temperature range . 334
5.10.1 Temperatures related to the maximum service temperature . 335
5.11 Electrical properties . 341
5.11.1 Electrical resistance and electrical resistivity . 341
5.12 Prelaunch environmental effects . 348
5.12.1 Moisture absorption and desorption . 348
5.13 Postlaunch environmental effects . 355
5.13.1 Ascent . 355
5.13.2 Orbital effects . 357
5.13.3 Re-entry effects . 367
5.14 Thermal vacuum cycling . 371
5.14.1 Test facilities . 371
5.14.2 Measurement methods . 372
5.14.3 Thermal vacuum cycling effects on the coefficient of linear thermal
expansion . 373
5.14.4 Trends in the variation of mechanical properties . 378
5.15 Coating application . 378
5.15.1 Pcbz conductive white paint . 378
5.15.2 APA-2474 (TiO white paint) . 378
2
3

---------------------- Page: 5 ----------------------
kSIST-TP FprCEN/CLC/TR 17603-31-05:2021
FprCEN/CLC/TR 17603-31-05:2021 (E)
5.15.3 Wiederhold's Z-12321 . 379
5.16 Past spatial uses . 380
5.16.1 Intelsat v . 380
5.16.2 Spelda (structure porteuse externe de lancement double ariane) . 381
5.16.3 CS-3A Japanese satellite . 384
Bibliography metalic materials . 387
References composite materials . 391

Figures
Figure 4-1: Specific heat, c, of Aluminium as a function of temperature, T. 30
Figure 4-2: Thermal conductivity, , of Aluminium as a function of temperature, T. . 31
Figure 4-3: Thermal conductivity integrals of Aluminium as a function of temperature, . . 32
Figure 4-4: Thermal diffusivity,  , of Aluminium as a function of temperature,  . . 33
Figure 4-5: Linear thermal expansion, L / L, of Aluminium as a function of
temperature, . 34
Figure 4-6: Normal spectral emittance,  ', of Aluminium as a function of wavelength, . . 37

Figure 4-7: Normal spectral emittance,  ', of Aluminium conversion coatings as a

function of wavelength, . . 38
Figure 4-8: Angular spectral emittance,  ', of Aluminium as a function of wavelength, . . 39

Figure 4-9: Normal total emittance, ', of Aluminium as a function of temperature, . . 45
Figure 4-10: Normal total emittance, ', of Aluminium anodized as a function of
anodizing thickness, t . . 46
c
Figure 4-11: Summary of data concerning the hemispherical total emittance, , of
Aluminium as a function of temperature, . From Touloukian & DeWitt
(1970) [42]. . 47
Figure 4-12: Summary of data concerning the hemispherical total emittance, , of
Aluminium conversion coatings vs. temperature, . From Touloukian,
DeWitt & Hernicz (1972) [43]. . 52
Figure 4-13: Directional spectral absorptance,  ', of Aluminium as a function of

wavelength, . Data points correspond to = 25°. . 54
Figure 4-14: Absorptance to emittance ratio,  /, of Aluminium conversion coatings as
s
a function of the exposure time, t. . 60
Figure 4-15: Normal - normal spectral reflectance,  '', of Aluminium as a function of

wavelength, . . 62
Figure 4-16: Normal - normal spectral reflectance,  '', of Aluminium contact coatings

as a function of wavelength, . . 64
Figure 4-17: Effect of coating thickness on normal - normal spectral reflectance,  '', of

Aluminium conversion coatings as a function of wavelength, . . 65
Figure 4-18: Bidirectional reflectance,  '', of Aluminium contact coatings as a function

of wavelength, . . 66
4

---------------------- Page: 6 ----------------------
kSIST-TP FprCEN/CLC/TR 17603-31-05:2021
FprCEN/CLC/TR 17603-31-05:2021 (E)
Figure 4-19: Bidirectional spectral reflectance,  '', of Aluminium conversion coatings

as a function of zenith angles,  and  ', of incident and reflected radiations. . 68
Figure 4-20: Summary of data concerning normal - hemispherical spectral reflectance,
 ', of Aluminium vs. wavelength, . From Touloukian & DeWitt (1970) [42]. . 69

Figure 4-21: Normal - hemispherical spectral reflectance,  ', of Aluminium conversion

coatings as a function of wavelength, . . 70
Figure 4-22: Effect of UV exposure on normal - hemispherical spectral reflectance,  ',

of Aluminium conversion coatings as a function of wavelength, . 71
Figure 4-23: Effect of electron exposure on normal - hemispherical spectral reflectance
of Aluminium conversion coatings as a function of wavelength, . 72
Figure 4-24: Effect of simultaneous UV - electron exposure on normal - hemispherical
spectral reflectance,  ', of Aluminium conversion coatings as a function of

wavelength, . . 73
Figure 4-25: Effect of proton exposure on normal - hemispherical spectral
reflectance,' , of Aluminium conversion coatings as a function of

wavelength,. . 74
Figure 4-26: Directional - hemispherical spectral reflectance,  ', of Aluminium

conversion coatings as a function of wavelength, . . 75
Figure 4-27: Hemispherical - normal spectral reflectance,  ', of Aluminium contact

coatings as a function of wavelength, . . 76
Figure 4-28: Bidirectional total reflectance, '', of Aluminium as a function of the viewing
zenith angles, '. . 77
Figure 4-29: Normal - normal spectral transmittance,  '', of Aluminium as a function of

wavelength, . . 80
Figure 4-30: Angular spectral transmittance,  '', of Aluminium as a function of

wavelength, . . 81

Figure 4-31: Electrical resistivity,  , of Aluminium as a function of temperature, . . 83
Figure 4-32: Specific heat, c, of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a function of
temperature, . 86
Figure 4-33: Thermal conductivity, k, of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a function of
temperature, . 87
Figure 4-34: Thermal conductivity integrals of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a
function of temperature, . . 88
Figure 4-35: Thermal diffusivity, , of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a function of
temperature, . 89
Figure 4-36: Linear thermal expansion, L / L, of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a
function of temperature, . . 90
Figure 4-37: Normal - spectral emittance,  ', of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a

function of wavelength, . . 91
Figure 4-38: Normal total emittance, ', of Al - 4,3 Cu - 1,5 Mg - 0,6 Mn as a function of
temperature, T. 93
Figure 4-39: Normal-normal spectral reflectance, '', of Al-4,3 Cu-1,5 Mg-0,6 Mn,
anodized, as a function of wavelength, . . 98
5

---------------------- Page: 7 ----------------------
kSIST-TP FprCEN/CLC/TR 17603-31-05:2021
FprCEN/CLC/TR 17603-31-05:2021 (E)
Figure 4-40: Normal - hemispherical spectral reflectance,  ', of Al - 4,3 Cu - 1,5 Mg -

0,6 Mn as a function of wavelength,  . 99
Figure 4-41: Normal - hemispherical spectral reflectance,  ', of Al - 4,3 Cu - 1,5 Mg -

0,6 Mn, anodized, as a function of wavelength, . . 100
Figure 4-42: Normal-hemispherical spectral reflectance,  ', of Al-1 Mg-0,6 Si, as

received, as a function of wavelength, . . 108
Figure 4-43: Normal-hemispherical spectral reflectance,  ', of Al-1 Mg-0,6 Si, grit

blasted, as a function of wavelength, . . 109
Figure 4-44: Normal-hemispherical spectral reflectance,  ', of Al-1 Mg-0,6 Si,

chemically polished, as a function of wavelength, . . 111
Figure 4-45: Normal - hemispherical spectral reflectance,  ', of Al - 1 Mg - 0,6 Si,

chemically milled, as a function of wavelength, . . 112
Figure 4-46: Specific heat, c, of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a function of
temperature, . 115
Figure 4-47: Thermal conductivity, k, of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a function of
temperature, T. 116
Figure 4-48: Thermal conductivity integral of Al – 5,7 Zn – 2,5 Mg – 1,6 Cu as a
function of temperature, T. . 117
Figure 4-49: Thermal diffusivity, , of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a function of
temperature, T. 118
Figure 4-50: Linear thermal expansion, L / L, of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a
function of temperature, . . 119
Figure 4-51: Normal spectral emittance,  ', of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a

function of wavelength,  . 120
Figure 4-52: Angular spectral emittance,  ', of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a

function of wavelength, . . 121
Figure 4-53: Normal total emittance, ', of Al - 5,7 Zn - 2,5 Mg - 1,6 Cu as a function of
temperature,. 122
Figure 4-54: Normal-hemispherical spectral reflectance, ' , of Al - 5,7 Zn - 2,5 Mg - 1,6

Cu conversion coatings, as a function of wavelngth, . . 126
Figure 4-55: Specific heat, c, of Ti - 5 Al - 2,5 Sn as a function of temperature, T. . 134
Figure 4-56: Thermal conductivity, k, of Ti - 5 Al - 2,5 Sn as a function of temperature,
T. 135
Figure 4-57: Thermal linear expansion, L/L, of Ti - 5 Al - 2,5 Sn as a function of
temperature, T. 136
Figure 4-58: Normal spectral emittance, ', of Ti - 5 Al - 2,5 Sn as a function of
7
temperature, T, for  =6,65 x 10 m. . 137
Figure 4-59: Normal total emittance, ', of Ti - 5 Al - 2,5 Sn as a function of
temperature, T. 138
Figure 4-60: Normal-normal spectral reflectance,  '', of Ti - 5 Al - 2,5 Sn as a function

of wavelength, . . 140
Figure 4-61: Normal - hemispherical spectral reflectance,  ', of Ti - 5 Al - 2,5 Sn as a

function of wavelength, . . 141
6

---------------------- Page: 8 ----------------------
kSIST-TP FprCEN/CLC/TR 17603-31-05:2021
FprCEN/CLC/TR 17603-31-05:2021 (E)
Figure 4-62: Normal - hemispherical spectral reflectance,  ', of Ti - 5 Al - 2,5 Sn,

anodized, as a function of wavelength, . . 142

Figure 4-63: Electrical resistivity,  , of Ti - 5 Al - 2,5 Sn as a function of temperature,
T. 143
Figure 4-64: Specific heat, c, of Ti - 6 Al - 2 Sn - 4 Zr - 2 Mo as a function of
temperature, T. 145
Figure 4-65: Thermal conductivity, k, of Ti - 6 Al - 2 Sn - 4 Zr - 2 Mo as a function of
temperature, T. 146
Figure 4-66: Mean coefficient of linear thermal expansion, , of Ti - 6 Al - 2 Sn - 4 Zr - 2
Mo from room temperature to temperature T. . 147

Figure 4-67: Electrical resistivity,  , of Ti - 6 Al - 2 Sn - 4 Zr - 2 Mo as a function of
temperature, T. 149
Figure 4-68: Specific heat, c, of Ti - 6 Al - 4 V as a function of temperature, T. . 152
Figure 4-69: Thermal conductivity, k, of Ti - 6 Al - 4 V as a function of temperature, T. . 153
Figure 4-70: Thermal conductivity integrals of Ti - 6 Al - 4 V as a function of
temperature, T. 154
Figure 4-71: Thermal diffusivity, , of Ti - 6 Al - 4 V as a function of temperature, T. . 155
Figure 4-72: Thermal linear expansion, L/L, of Ti - 6 Al - 4 V as a function of
temperature, T. 156
Figure 4-73: Normal spectral emittance,  ', of Ti - 6 Al - 4 V as a function of

temperature, T. 157
Figure 4-74: Normal total emittance, ', of Ti - 6 Al - 4 V as a function of temperature, T. . 158
Figure 4-75: Hemispherical total emittance, , of Ti - 6 Al - 4 V as a function of
temperature, T. 160
Figure 4-76: Normal - hemispherical spectral reflectance,  ', of Ti - 6 Al - 4 V as a

function of wavelength, . . 162

Figure 4-77: Electrical resistivity,  , of Ti - 6 Al - 4 V as a function of temperature, T. . 163
Figure 4-78: Specific heat, c, of Ni - 19 Cr - 11 Co - 10 Mo - 3 Ti as a function of
temperature, T. 166
Figure 4-79: Thermal conductivity, k, of Ni - 19 Cr - 11 Co - 10 Mo - 3 Ti as a function
of temperature, T. . 167
Figure 4-80: Thermal linear expansion, L/L, of Ni - 19 Cr - 11 Co - 10 Mo - 3 Ti as a
function of temperature, T. . 168
Figure 4-81: Normal spectral emittance,  ', of Ni - 19 Cr - 11 Co - 10 Mo - 3 Ti as a

function of wavelength, . . 169
Figure 4-82: Normal total emittance, ', of Ni - 19 Cr - 11 Co - 10 Mo - 3 Ti as a function
of temperature, T. . 170
Figure 4-83: Normal-normal spectral reflectance, " , of Ni - 19 Cr - 11 Co - 10 Mo - 3

Ti as a function of wavelength, . Data points correspond to normal-
hemispherical reflectance while , , correspond to hemispherical-normal
reflectance. . 172
Figure 4-84: Specific heat, c, of Fe - 36 Ni (Invar) as a function of temperature, T. . 176
7

---------------------- Page: 9 ----------------------
kSIST-TP FprCEN/CLC/TR 17603-31-05:2021
FprCEN/CLC/TR 17603-31-05:2021 (E)
Figure 4-85: Linear thermal expansion, L/L, of Fe - 36 Ni (Invar) as a function of
temperature, T. 177
Figure 4-86: Effect of the concentration of alloying elements, c, on the value of the
coefficient of linear expansion, . From MOND NICKEL Co. . 178
7
Figure 4-87: Normal emittance,  ', of Fe - 36 Ni (Invar), for  = 6,7 x 10 as a function

of temperature, T. . 179
Figure 5-1: International ties between Carbon Fiber manufactures. From SENER
(1984) [147]. . 205
Figure 5-2: Schematic of an angle plied laminate. From Chamis (1987) [67]. . 206
Figure 5-3: Schematic of a tri-orthogonally fiber reinforced composite. a) Straight
filaments. From Domínguez (1987) [82]. b) Tapes. From Aboudi (1984)
[49]. . 206
Figure 5-4: Main types of woven fabrics. Lengthwise (warp) yarns and crosswise (fill)
yarns can be interlaced to produce woven fabrics. A fabric construction of
16 x 14 means 16 warp ends per inch and 14 fill ends per inch. a) Plain
weave. Very stable. Small yarn slippage. b) Leno weave. Minimizes
distortion with few yarns. c) Twill. The fabric has a broken diagonal line
and, consequently, greater pliability than a plain weave. d) Crowfoot satin.
Pliable and confortable to contoured surfaces. From Domínguez (1987)
[82], Weeton, Peters & Thomas (1987) [164]. . 207
Figure 5-5: Longitudinal (to fibers) and transverse directions for the measurement of
composite properties. From Chamis (1987) [67]. . 209
Figure 5-6: Cryostat assemblies for measuring the thermal conductivity, k. a) High-k
samples. b) Low-k samples. F
...

Questions, Comments and Discussion

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