Pegasus XL | Fast On-orbit Rapid Recording of Transient Events (FORTE)

Pegasus XL | Fast On-orbit Rapid Recording of Transient Events (FORTE) rode a Pegasus XL into space from Vandenberg SFB, CA, USA, deploying its payload to the designated orbit.

Launch time
Status
SUCCESS
Operator
Orbital Sciences Corporation
Mission type
Orbital
Launch pad
Space Launch Complex 10E
Payload
—
Target orbit
Unknown
Pegasus XL | Fast On-orbit Rapid Recording of Transient Events (FORTE) cover image

Mission timeline

  1. 1997-08-29T15:02:22.000Z
    Liftoff
    Pegasus XL roars off the pad at Vandenberg SFB, CA, USA.
  2. Max-Q
    The vehicle reaches Max Q, the highest aerodynamic load of the flight.
  3. Main engine cutoff (MECO)
    MECO — first-stage propulsion ends after a nominal burn.
  4. Stage separation
    Clean stage separation confirmed.
  5. Second-stage ignition
    The upper-stage engine lights up after separation.
  6. Mission success
    All mission objectives achieved.

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