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T+255: NSSL Phase 3 Addendum
Main Engine Cut Off
The Revised Target for Satellite Launches
The offers proposed launch systems is capable of achieving at least fifteen thousand pounds massed orbit five hundred article miles circular orbits sixty three point four degree inclination with orbital accuracy probability dot a dot a dot as defined in these other documents. This can be achieved with a single launch or multiple launches minimum of one thousand kilograms per launch and multiple launch configurations. So they are now revising that target from i think it was eight tons before is what your back told me but now it's at six point eight metric tons uh... It does open up the range of new launch vehicles though it's getting trimmed with relativity having canceled turn one.
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