Mu-3S-II | Yohkoh

A Mu-3S-II rocket launched Mu-3S-II | Yohkoh from Uchinoura Space Center, Japan, targeting LEO.

Launch time
Status
SUCCESS
Operator
Institute of Space and Astronautical Science
Mission type
Earth Science
Rocket
Mu-3S-II
Launch site
Uchinoura Space Center, Japan
Launch pad
Mu Center
Payload
—
Target orbit
LEO

Mission timeline

  1. 1991-08-30T02:30:00.000Z
    Liftoff
    Liftoff confirmed — Mu-3S-II is airborne.
  2. Max-Q
    Max Q — Mu-3S-II endures peak structural stress during ascent.
  3. Main engine cutoff (MECO)
    First-stage main engine cutoff (MECO) confirmed.
  4. Stage separation
    The spent first stage separates from the upper stage.
  5. Second-stage ignition
    Upper stage ignites, continuing the journey toward orbit.
  6. Orbit insertion
    The mission reaches LEO, successfully entering orbit.
  7. Mission success
    The mission concludes successfully.

Last updated: