PPT Slide

IMAGE ELV Configuration

and Mission Characteristics

• Vehicle Configuration: Boeing Delta Medium-Lite

7326-9.5

- Same as Deep Space-1 with exception

of mission specific mods

• Launch Site: SLC-2W at VAFB

• Launch Period: February 15 thru March 10,

2000 based on current trajectory analysis

• Liftoff time (hr:min:sec PST)

  • 15 Feb 00 14:02:15
    

• Orbit Requirements

  • Apogee Altitude (km/nmi) 45923.2/24796.5
  • Perigee Altitude (km/nmi) 1000/540
  • Inclination (deg) 90
  • Argument of Perigee (deg) 320

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