TNI CEN/CLC/TR 17603-31-10
| Name: | TNI CEN/CLC/TR 17603-31-10 |
| Validity: | Valid |
| Number of pages: | 128 |
| Language: |
EN
|
| Paper: | 35,00€ |
| Electronic version |
a) Only read (without ability to print and copy)
31,50€ b) Without ability to print, with ability to copy (printscreen) 35,00€ c) With ability to print and copy (printscreen) 45,50€ |
| Slovak title | Kozmická technika. Príručka pre tepelnotechnický návrh. Časť 10: Kondenzátor s fázovou premenou |
| English title | Space engineering - Thermal design handbook - Part 10: Phase - Change Capacitor |
| Release Date: | 01. 01. 2022 |
| Date of withdrawal: | |
| ICS: | 49.140 |
| Sorting character/National clasification code | 31 0540 |
| Level of incorporation: | idt CEN/CLC/TR 17603-31-10:2021 |
| Official Journal | 12/21 |
| Amendments | |
| Replaced by: | |
| Repleces: | |
| Note in Official Journal: | |
| Subject of the standard: | Solid-liquid phase-change materials (PCM) are a favoured approach to spacecraft passive thermal control for incident orbital heat fluxes or when there are wide fluctuations in onboard equipment. The PCM thermal control system consists of a container which is filled with a substance capable of undergoing a phase-change. When there is an the increase in surface temperature of spacecraft the PCM absorbs the excess heat by melting. If there is a temperature decrease, then the PCM can provide heat by solidifying. Many types of PCM systems are used in spacecrafts for different types of thermal transfer control. Characteristics and performance of phase control materials are described in this Part. Existing PCM systems are also described. 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 |
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