Spacecraft Thermal Control Handbook, VolumeI: Fundamentals Technologies

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 |