Low cost thermal-vacuum system for the development of very small spacecraft

Tatsuo Shimizu, Takuya Motohata, Hirokazu Masui, Minoru Iwata, Mengu Cho, Johnny Finnholm, Antti Kestilä

    Research output: Chapter in Book/Report/Conference proceedingConference contributionScientificpeer-review

    Abstract

    Simulated space environments are necessary for validating the functionality of spacecraft and/or payloads during their development phase. A thermal-vacuum chamber is a key space environment simulator. Conventional chambers provide a high vacuum environment as well as thermal cycle environments that provide conditions similar to those encountered in space. However, even small such chambers are expensive, and are often beyond the budget of a university-based space project. In addition, the need to use liquid nitrogen coolant adds an additional high running cost. For this reason, we developed a small thermal vacuum test facility that costs less than 2000USD and which uses solid-state Peltier heaters/coolers.

    Original languageEnglish
    Title of host publication65th International Astronautical Congress 2014, IAC 2014: Our World Needs Space
    PublisherInternational Astronautical Federation, IAF
    Pages5903-5906
    Number of pages4
    Volume8
    ISBN (Electronic)9781634399869
    Publication statusPublished - 2014
    MoE publication typeA4 Article in a conference publication
    EventInternational Astronautical Congress - Toronto, Canada
    Duration: 29 Sep 20143 Oct 2014
    Conference number: 65

    Conference

    ConferenceInternational Astronautical Congress
    Abbreviated titleIAC
    CountryCanada
    CityToronto
    Period29/09/201403/10/2014

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