Ablative cooling.What kind of cooling is on that exhaust cone?
Ablative cooling.What kind of cooling is on that exhaust cone?
Did anyone else start to get concerned about the exhaust cone glowing red...it looked like it was going to disintegrate at one point! The commentator did say that was normal, though. What kind of cooling is on that exhaust cone?
Thanks for the correction.Ablative throat, radiatively cooled nozzle.
http://spacex.com/falcon1.php
So? Would still be cool to see it in free fall.
Did anyone else start to get concerned about the exhaust cone glowing red...it looked like it was going to disintegrate at one point! The commentator did say that was normal, though. What kind of cooling is on that exhaust cone?
If anyone finds a youtube of this, please post.
Um. Velocity relative to what?
At the moment of orbit, they have 5500 m/s, how is that?
What's the price of the launch in per kg of payload?

Strange. 5200 m/s is too slow for a 315km orbit.
Strange. 5200 m/s is too slow for a 315km orbit. But it's too slow after cut off anyway.
No aborts, or unexpected holds or anything
SECO! What a great moment! The first private rocket in Orbit!

I thought it was in a 600km orbit?
Not that 5200m/s is good for that either.
The JSR has the Falcon 1 second stage with "RatSat" in a 621x643 kmx9.3° orbit: http://planet4589.org/space/jsr/latest.htmlIf they placed a dummy payload into Orbit, the payload is space debris and should appear in the TLE files soon.