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Patent Searching and Data


Title:
ナノサットの電熱展開システム
Document Type and Number:
Japanese Patent JP6745590
Kind Code:
B2
Abstract:
An electrothermal deployment system (40) may be configured for controlled release of various apparatus (20) from their prelaunch stowage positions in small satellites (10). The deployment system includes a fusible line (60) secured to a structural component (20) of the satellite, as well as to various deployable apparatus secured to, within, or on the satellite. The deployable apparatus may include items such as solar panels (20) and antennas. The deployment system includes an electrically resistive element ((42) such as a burn bar formed of a cylinder or tube, including a resistor pad (44) overlying and/or incorporated within an exterior surface of the burn bar (42). The burn bar may be coupled to an electrical circuit configured to heat the resistor for the purpose of melting the fusible line secured in direct contact therewith, thus causing the fusible line to break to cause deployment. The fusible line is configured to remain in secure contact with the resistor until apparatus deployment.

Inventors:
Jeffrey Orias
Michael Worcester
John Behrens
Bruce El Doloren
Application Number:
JP2015159831A
Publication Date:
August 26, 2020
Filing Date:
August 13, 2015
Export Citation:
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Assignee:
The Boeing Company
International Classes:
B64G1/22; B64G1/44; H05B3/00
Foreign References:
WO2013049588A1
US20060088366
US6439122
Other References:
J. Bouwmeester, G. T. Aalbers, W. J. Ubbels,PRELIMINARY MISSION RESULTS AND PROJECT EVALUATION OF THE DELFI-C3 NANO-SATELLITE,Proceedings of the 4S Symposium,NL,European Space Agency,2008年,ISBN:978-92-9221-224-7
Alphonso C. Stewart and Jason H. Hair,Intricacies of Using Kevlar Cord and Thermal Knives in a Deployable Release System: Issues and Solutions,Proceedings of the 36th Aerospace Mechanisms Symposium,米国,2002年,pp.243-255
Attorney, Agent or Firm:
Yasuhiko Murayama
Tatsuhiko Abe
Kuroda Shinpei
Choi