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BSI PD CEN/CLC/TR 17603-31-05:2021

$215.11

Space Engineering. Thermal design handbook – Structural Materials: Metallic and Composite

Published By Publication Date Number of Pages
BSI 2021 402
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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 Thermal design handbook – Part 1: View factors

TR 17603-31-02 Thermal design handbook – Part 2: Holes, Grooves and Cavities

TR 17603-31-03 Thermal design handbook – Part 3: Spacecraft Surface Temperature

TR 17603-31-04 Thermal design handbook – Part 4: Conductive Heat Transfer

TR 17603-31-05 Thermal design handbook – Part 5: Structural Materials: Metallic and Composite

TR 17603-31-06 Thermal design handbook – Part 6: Thermal Control Surfaces

TR 17603-31-07 Thermal design handbook – Part 7: Insulations

TR 17603-31-08 Thermal design handbook – Part 8: Heat Pipes

TR 17603-31-09 Thermal design handbook – Part 9: Radiators

TR 17603-31-10 Thermal design handbook – Part 10: Phase – Change Capacitors

TR 17603-31-11 Thermal design handbook – Part 11: Electrical Heating

TR 17603-31-12 Thermal design handbook – Part 12: Louvers

TR 17603-31-13 Thermal design handbook – Part 13: Fluid Loops

TR 17603-31-14 Thermal design handbook – Part 14: Cryogenic Cooling

TR 17603-31-15 Thermal design handbook – Part 15: Existing Satellites

TR 17603-31-16 Thermal design handbook – Part 16: Thermal Protection System

PDF Catalog

PDF Pages PDF Title
2 undefined
20 1 Scope
21 2 References
22 3 Terms, definitions and symbols
3.1 Terms and definitions
3.2 Symbols
25 4 Metallic materials
4.1 General
28 4.1.1 Modifiers of thermal radiative properties
29 4.1.2 Cladding definitions
30 4.1.3 Temper designation for heat treatable aluminium alloys
4.2 Aluminium alloys
87 4.3 Aluminium-Copper alloys
106 4.4 Aluminium-Magnesium alloys
116 4.5 Aluminium-Zinc alloys
133 4.6 Magnesium-Zink-Thorium alloys
135 4.7 Titanium-Aluminium-Tin alloys
146 4.8 Titanium-Aluminium-Tin alloys
153 4.9 Titanium-Aluminium-Vanadium alloys
167 4.10 Nickel-Chrome-Cobalt-Molybdenum alloys
177 4.11 Iron-Nickel alloys
184 5 Composite materials
5.1 List of symbols
189 5.2 List of matrices, prepregs and laminates quoted in this clause
190 5.2.1 Matrices, adhesives, potting, moulding compounds
195 5.2.2 Prepregs, laminates and films
197 5.2.3 Code list of manufacturers (or developers)
199 5.3 General introduction
200 5.3.2 Composition
5.3.2.1 Reinforcements
201 5.3.2.2 Matrices
202 5.3.3 Commercial fiber product names, descriptions and manufacturers
207 5.3.4 Geometry of fiber reinforcement. fabrics. abridged designation
212 5.4 Physical properties
5.4.1 Density
5.4.1.1 Calculation formula for composites
5.4.1.2 Tabulated data
218 5.5 Thermal properties
5.5.1 Specific heat
5.5.1.1 Measuring methods
5.5.1.2 Calculation formula for composites
224 5.5.2 Thermal conductivity
5.5.2.1 Measuring methods
227 5.5.2.2 Calculation formulae for composites
228 5.5.2.3 Tabulated data
249 5.5.3 Thermal diffusivity
5.5.3.1 Measuring methods
251 5.5.3.2 Tabulated data
258 5.6 Thermo-elastic properties
5.6.1 Coefficient of linear thermal expansion
5.6.1.1 Measuring methods
261 5.6.1.2 Calculation formulae for composites
262 5.6.1.3 Tabulated data
321 5.7 Thermal radiation properties of bare high strength fibers
5.7.1 Sample characterization
5.7.2 Emittance
5.7.2.1 Hemispherical total emittance
323 5.7.3 Absorptance
5.7.3.1 Solar absorptance
5.7.3.2 Influence of the substrate on the solar absorptance
324 5.7.3.3 Solar absorptance of mosaics
325 5.7.3.4 Effects of the space environment on absorptance
326 5.8 Thermal radiation properties of bare composite materials
5.8.1 Tabulated data
328 5.9 Thermal radiation properties of coated composite materials
329 5.9.1 White painted composite materials
5.9.1.2 Normal spectral emittance
330 5.9.1.3 Normal total emittance
331 5.9.1.4 Normal-hemispherical spectral reflectance
332 5.9.1.5 Normal solar reflectance
333 5.9.2 Sputtered Aluminium on graphite-epoxy composite material
5.9.2.1 Normal total emittance
334 5.9.2.2 Solar absorptance
336 5.9.2.3 Solar absorptance to emittance ratio
5.10 Operating temperature range
337 5.10.1 Temperatures related to the maximum service temperature
343 5.11 Electrical properties
5.11.1 Electrical resistance and electrical resistivity
5.11.1.1 Calculation formulae for composites
344 5.11.1.2 Tabulated data
346 5.11.1.3 High-frequency effects
347 5.11.1.4 Electrical behaviour of structural joints
350 5.12 Prelaunch environmental effects
5.12.1 Moisture absorption and desorption
5.12.1.2 Fickian analysis of moisture absorption of composite materials
354 5.12.1.3 Maximum moisture content. Experimental data
355 5.12.1.4 Transverse coefficient of diffusion. Experimental data
356 5.12.1.5 Trends in the variation of mechanical properties
357 5.13 Postlaunch environmental effects
5.13.1 Ascent
5.13.1.1 Outgassing
359 5.13.2 Orbital effects
360 5.13.2.1 Test facilities
361 5.13.2.2 Measurement methods
362 5.13.2.3 Radiation effects on the coefficient of linear thermal expansion
365 5.13.2.4 Trends in the variation of mechanical properties
366 5.13.2.5 Atomic oxygen effects
369 5.13.3 Re-entry effects
5.13.3.1 Oxidation
373 5.14 Thermal vacuum cycling
5.14.1 Test facilities
374 5.14.2 Measurement methods
375 5.14.3 Thermal vacuum cycling effects on the coefficient of linear thermal expansion
380 5.14.4 Trends in the variation of mechanical properties
5.15 Coating application
5.15.1 Pcbz conductive white paint
5.15.2 APA-2474 (TiO2 white paint)
381 5.15.3 Wiederhold’s Z-12321
5.15.3.1 General
5.15.3.2 Filling
5.15.3.3 Priming
5.15.3.4 Thinning
5.15.3.5 Antierosion coating
382 5.15.3.6 Finishing coating
5.16 Past spatial uses
5.16.1 Intelsat v
383 5.16.2 Spelda (structure porteuse externe de lancement double ariane)
386 5.16.3 CS-3A Japanese satellite
BSI PD CEN/CLC/TR 17603-31-05:2021
$215.11