Experimental investigation of a passive deployable/stowable radiator

Hosei Nagano, Akira Ohnishi, Ken Higuchi, Yu Oikawa, Kazuki Watanabe, Yuji Nagasaka

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

A passive delployable/stowable radiator named reversible thermal panel (RTP) has been developed for thermal control of interplanetary spacecrafts. The RTP can autonomously adapt to a wide variety of thermal environments with no electrical power. An RTF prototype model (PM) was fabricated and extensive test programs including fin deployment/stowing tests, thermal performance tests, and vibration tests have been executed to validate that the RTP-PM can meet all the qualification requirements. Deployment/stowing tests have demonstrated repeatable RTF fins deploy/stow from 0° to 140° over the temperature range from -30°C to +30°C. Thermal performance tests including thermal balance tests and power cycling tests have shown RTF's autonomous thermal control for changes in thermal conditions. The RTF has also been subjected to qualification-level vibration loads and passed with no significant issues.

Original languageEnglish
Title of host publicationCollection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
Pages14506-14514
Number of pages9
Volume21
Publication statusPublished - 2007
Event45th AIAA Aerospace Sciences Meeting 2007 - Reno, NV, United States
Duration: 2007 Jan 82007 Jan 11

Other

Other45th AIAA Aerospace Sciences Meeting 2007
CountryUnited States
CityReno, NV
Period07/1/807/1/11

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ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Nagano, H., Ohnishi, A., Higuchi, K., Oikawa, Y., Watanabe, K., & Nagasaka, Y. (2007). Experimental investigation of a passive deployable/stowable radiator. In Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting (Vol. 21, pp. 14506-14514)