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MABES + R/B

NSSDCA/COSPAR ID: 1986-061C

Description

MABES (Magnetic Bearing Flywheel Experimental System) was launched by a two-stage H-I launch vehicle from the Tanegashima Space Center of the National Space Development Agency of Japan. The national name of the satellite was Jindai. Its mission was to measure levitating/oscillatory/rotating characteristics of the magnetic bearing flywheel under zero G conditions and to confirm the function of the launch lock mechanism.

Alternate Names

  • Jindai
  • 16910
  • Mag Bearing Flywheel Exp
  • MABES+R/B
  • 1986-061C

Facts in Brief

Launch Date: 1986-08-12
Launch Vehicle: H-I
Launch Site: Tanegashima, Japan

Funding Agency

  • Unknown Japan

Discipline

  • Engineering

Additional Information

Questions and comments about this spacecraft can be directed to: Coordinated Request and User Support Office

 

Personnel

NameRoleOriginal AffiliationE-mail
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