Spacecraft Thermal Control Handbook, VolumeI: Fundamentals Technologies

Appendix B: Material Thermal Properties

Overview

The room-temperature material property values contained in this appendix were obtained from a variety of sources. While the values shown are believed to be accurate, no guarantee of their validity is implied. In cases where a thermal design is sensitive to any of these parameters, material property tests and/or a design thermal balance test must be conducted to verify flight performance.

Solid Material Thermal Properties

Material

? (kg/cm 3)

k (W/cm C)

c p ( W-hr/kg C )

Aluminum

208

0.00277

1.212

222

0.00277

1.333

242

0.00277

1.506

295

0.00277

1.437

B295.0

0.00277

1.610

308

0.00277

1.419

319

0.00277

1.142

355

0.00277

1.506

C355.0

0.00277

1.419

356

0.00277

1.593

A356.

0.00277

1.593

A380.

0.00277

1.004

A413.0

0.00277

1.212

443

0.00277

1.454

B443.0

0.00277

1.471

514

0.00277

1.385

518

0.00277

0.969

520

0.00277

0.883

D712.0

0.00277

1.385

1060-0

0.00277

2.354

1060-H18

0.00277

2.302

1100-0

0.00277

2.216

0.256

1100-H18

0.00277

2.216

1350-0

0.00277

2.337

2011-0

0.00277

1.437

0.267

2011-T3

0.00277

1.506

2011-T8

0.00277

1.714

2014-0

0.00277

1.887

0.256

2014-T4

0.00277

1.333

2014-T6

0.00277

1.558

2017-0

0.00277

1.921

0.256

2024-0

0.00277

1.887

0.256

2024-T3

0.00277

1.212

2024-T36

0.00277

1.212

2024-T4

0.00277

1.212

2024-T6

0.00277

1.212

2025-T6

0.00277

1.558

2036-0

0.00277

1.593

2219-0

0.00277

1.731

3003-0

0.00277

1.766

0.256

3003-H18

0.00277

1.766

3004-0

0.00277

1.627

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