Mission Objective

  The objective of this mission is functional test of communication antenna deployment mechanism developed for TITech CubeSat CUTE-I. CUTE-I has 430MHz band CW-transmitter, 430MHz band FM-transmitter and 140MHz band receiver. Thus three deployable monopole antennas are equipped. These antennas are fixed to structure of CUTE-I by Nylon line.
Nylon line attached to the tip of communicaton antenna is fixed like in left figure. Nichrome wire is winded in a spiral and nylon line is threaded into it.
Nichrome wire is heated turning on an electrical current to nichrome wier
Nylon line is melted and cut off, afterward communication antenna is deployed by own elasticity

  Therefor we load these components into TITech CarrierSat and conduct functional test of this mechanism during CarrierSat operating parasailling mission.



Laboratory for Space Systems in Tokyo Institute of Technology
LSS:
http://horse.mes.titech.ac.jp
email:Arliss2001 Team