Hi All: Here are some parameters for next week's Delta II/NOAA-N launch from California: Launch Date: 2005 May 11 Launch Time: 10:22:01 UTC/03:22:01 PDT Launch Site: Vandenberg AFB SLC-2W Launch Vehicle: Delta II with three (not nine) strap-on solid motors Flight Events: Event T+ (sec) ------------------------- -------- Liftoff 000.0 Solid motot burnout 060.0 Solid motor separation 099.0 Main engine cutoff 264.2 1/2 separation 272.2 Stage 2 ignition 277.7 Jettison faring 296.0 Sustainer engine cutoff 1 676.0 The above info may be generic and not computed for this specific launch Orbital Altitude: 870 km Orbital Inclination: 98.730° Orbital Period: 102.14 minutes Regards, Brian Webb www.spacearchive.info ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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