Databases

• Databases
  • Component catalog
    • Reaction Wheel Assenmbly Type M-A
    • Reaction Wheel Assenmbly Type L-A
    • Next Generation GPS Reciever
    • Reaction Wheel Assenmbly Type S
    • Inertial Reference Unit (IRU) Type III-C
    • XMOD (X-band Multi-mode High Speed Modulator)
    • MTP (Multi-mode Integrated Transponder: USB/QPSK mode)
    • MTP (Multi-mode Integrated Transponder: 4 mode)
    • High-performance Lithium-ion Cell for Space Applications (JMG190)(190Ah)
    • High-performance Lithium-ion Cell for Space Applications (JMG110)(110Ah)
    • High-performance Lithium-ion Cell for Space Applications (JMG055)(55Ah)
    • High-performance Lithium-ion Cell for Space Applications (JMG042)(42Ah)
    • High-performance Lithium-ion Cell for Space Applications (JMG150)(150Ah)
    • Lithium-ion Cell for Space Applications (JMG100)(100Ah)
    • Lithium-ion Cell for Space Applications (JMG050)(50Ah)
    • 20 N-class Thruster Valve
    • Latching Valve with Reverse Pressure Relief Function
    • Low Shock Release Device (LSRD-10K/C-2000)
    • Light-weight Harmonic Drive Gear (CSD-20-160-2A-GR-SP)
    • Harmonic Drive Gear (SHF-20-160-2A-GR-SP)
    • Resolver (TS2511)

High-performance Lithium-ion Cell for Space Applications (JMG055)(55Ah)

Registration date	4/14/2017
JAXA development group	Research Unit I, Research and Development Directorate
View diagram	See Attachment 1
Environmental resistance	See Attachment 2
Patent number (publication number)	N/A
Reference	N/A
Satellite and launch date	To be supplied after launch
Note	N/A

Manufacturer

GS Yuasa Technology Ltd.
Kyoto-shi, Kyoto, Japan
https://www.gs-yuasa.com/gyt/jp/

Features

• Long mission life
  ■ LEO 7 years
  ■ GEO 20 years
• Higher specific energy
  150 Wh/kg (Typical)

Applications

Supply of electric power to a satellite/probe when solar power is not available (eclipse period).

Specifications