MABES

MABES
Mission typeTechnology development/test satellite
OperatorNASDA
COSPAR ID1986-061C
SATCAT no.16910
Start of mission
Launch date12 August 1986, 20:45 (1986-08-12UTC20:45Z) UTC
RocketH-I
Launch siteTanegashima Osaki
ContractorMitsubishi
End of mission
DisposalDecommissioned
Orbital parameters
Reference systemGeocentric
Regimelow Earth
Perigee altitude1,489.6 kilometres (925.6 mi)
Apogee altitude1,061.8 kilometres (659.8 mi)
Inclination50.0 degrees
Period116.8 minutes
 

Magnetic Bearing Flywheel Experimental System (MABES), also known as Jindai (じんだい) is a National Space Development Agency of Japan(NASDA) satellite mission. It conducted experiments on the levitation of the magnetic bearing flywheel in a zero-G environment, and tested the function of the launch lock mechanism.

On 12 August 1986, Jindai was launched from Tanegashima Space Center aboard the maiden flight of H-I rocket, along with Ajisai and Fuji.

Jindai is attached to the second stage of the H-1 rocket, and as of 2013, still remains in low Earth orbit.

References

  1. ^ a b c d e "H-1 R/B(MABES)". REAL TIME SATELLITE TRACKING. Retrieved 2010-03-18.
  2. ^ "Past Projects - Satellites and Spacecraft". JAXA. Retrieved 2015-10-16.
  3. ^ "MABES (Jindai)". GUNTER'S SPACE PAGE. Retrieved 2013-08-13.