Jindai

Japan


International Sat. n°:

Japanese satellite n°: 42

Orig PL Name: MABES (MAgnetic Bearing flywheel Experimental System)

Launch data:

Designation 16910 / 86061C
Launch date12 Aug 1986 - 20:45 UT
Launch siteTanegashima
Launch vehicle: H1 (#H-15)
MissionScientific
Earth orbit on:
Perigee/Apogee1484 / 1594 km
Inclination50.00°
Period 115.7 min

MABES stayed attached to 2nd stage No 3nd stage?

Specifications:

Mass at launch 2400 kg
Diameter m
Stabilization passive


01 Jan 1986: EGS, MABES, JAS-1 after attaching to the rocket in the service tower - Credit: JAXA



Ref: #102, #235 - update: 08.09.10