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LIVE: ST5 Mission - March 22 2006
by
John44
on 13 Mar, 2006 10:15
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#1
by
Chris Bergin
on 13 Mar, 2006 12:45
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#2
by
jcm
on 13 Mar, 2006 13:04
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But no press kit as far as I can see? Does anyone have one?
I assume the planned drop point is the usual 36.0N 123.0W ?
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#3
by
Jim
on 13 Mar, 2006 14:47
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#4
by
DaveS
on 13 Mar, 2006 16:11
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Mission delayed 24 hrs to Wednesday due to predicted unfavorable weather conditions on Tuesday. 80% chance of favorable weather on Wednesday.
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#5
by
Chris Bergin
on 13 Mar, 2006 16:55
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DaveS - 13/3/2006 5:11 PM
Mission delayed 24 hrs to Wednesday due to predicted unfavorable weather conditions on Tuesday. 80% chance of favorable weather on Wednesday.
We can live with that.
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#6
by
jcm
on 13 Mar, 2006 22:36
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Thanks. I see the link on the NASA HQ site now. Could have sworn it wasn't there
when I looked this morning :-). Oh well...
Some nice things in the press kit. Spacecraft dimensions 0.53m dia 0.48m high stowed, mass 25 kg fully fuelled. Planned orbit 300 x 4500 km x 97 deg.
Drop at 12.2 km altitude.
Timeline: Drop+0:05 stage 1 burn, +1:17 stage 1 burnout at 55 km, +1:31 stage 2 burn at 72 km, +2:11 fairing sep at 115 km, +3:06 stage 2 burnout at 156 km,
+5:03 stage 3 burn at 283 km, +6:11 stage 3 burnout at 302 km, +9:31 ST5-FWD sep, +12:41 ST5-MID sep, +15:51 ST5-AFT sep.
GSFC has in-house prime contractor/integrator role, as far as I can tell.
Some things not in the press kit, but maybe someone here knows:
- Dry mass of spacecraft (or equally good, mass of propellant loaded)
- Drop point coords
- Nominal delta-v of stage 3 burn
- Span of spacecraft once boom is deployed (I guess about 1.0 meter)
- WHAT ARE THE THREE S/C GOING TO BE CALLED ONCE ON ORBIT? The only hint in the press kit is the
diagram calling them FWD, MID and AFT. But maybe they have serial numbers like S/N 1,2,3? and maybe they will be
given individual names (Larry, Curly, Moe? :-)). Any clues?
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#7
by
Jim
on 14 Mar, 2006 01:05
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jcm - 13/3/2006 5:36 PMThanks. I see the link on the NASA HQ site now. Could have sworn it wasn't therewhen I looked this morning :-). Oh well... Some nice things in the press kit. Spacecraft dimensions 0.53m dia 0.48m high stowed, mass 25 kg fully fuelled. Planned orbit 300 x 4500 km x 97 deg.Drop at 12.2 km altitude.Timeline: Drop+0:05 stage 1 burn, +1:17 stage 1 burnout at 55 km, +1:31 stage 2 burn at 72 km, +2:11 fairing sep at 115 km, +3:06 stage 2 burnout at 156 km,+5:03 stage 3 burn at 283 km, +6:11 stage 3 burnout at 302 km, +9:31 ST5-FWD sep, +12:41 ST5-MID sep, +15:51 ST5-AFT sep.GSFC has in-house prime contractor/integrator role, as far as I can tell.Some things not in the press kit, but maybe someone here knows: - Dry mass of spacecraft (or equally good, mass of propellant loaded) - Drop point coords - Nominal delta-v of stage 3 burn- Span of spacecraft once boom is deployed (I guess about 1.0 meter)- WHAT ARE THE THREE S/C GOING TO BE CALLED ONCE ON ORBIT? The only hint in the press kit is thediagram calling them FWD, MID and AFT. But maybe they have serial numbers like S/N 1,2,3? and maybe they will begiven individual names (Larry, Curly, Moe? :-)). Any clues?
56 lbs
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#8
by
Jim
on 14 Mar, 2006 01:36
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GN2 is the propellant
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#9
by
John44
on 14 Mar, 2006 05:09
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NASA'S ST5 LAUNCH POSTPONED DUE TO WEATHER FORECAST
Predicted weather conditions postponed Tuesday's scheduled launch of
NASA's Space Technology 5 (ST5) spacecraft. It will launch Wednesday,
March 15, at 9:02 a.m. EST.
The forecast improves on Wednesday with only a 20 percent chance of
not having acceptable weather.
ST5 launch coverage on NASA TV begins Wednesday at 7:30 a.m. EST. NASA
TV's Public
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#10
by
jcm
on 14 Mar, 2006 13:01
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| 56 lbs
Are you sure? , 56 lbs is the fully fuelled mass according to the sources I've seen, not the dry mass.
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#11
by
Jim
on 14 Mar, 2006 15:26
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jcm - 14/3/2006 8:01 AM| 56 lbsAre you sure? , 56 lbs is the fully fuelled mass according to the sources I've seen, not the dry mass.
For the size of the spacecraft, how much GN2 do you think they can compress to really make a difference? There isn't a "dry" or "wet" mass, since it uses GN2.
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#12
by
John44
on 14 Mar, 2006 16:55
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#13
by
Jim
on 14 Mar, 2006 17:48
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#14
by
jcm
on 14 Mar, 2006 22:01
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Jim - 14/3/2006 11:26 AM
jcm - 14/3/2006 8:01 AM| 56 lbsAre you sure? , 56 lbs is the fully fuelled mass according to the sources I've seen, not the dry mass.
For the size of the spacecraft, how much GN2 do you think they can compress to really make a difference? There isn't a "dry" or "wet" mass, since it uses GN2.
Ahh, good point. Wasn't thinking straight.
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#15
by
DaveS
on 15 Mar, 2006 11:19
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Everything looking good for a a launch today. L-1011 take-off is planned for 8:04 am EST, 1304 UTC. Weather is predicted to be 100% go at Pegasus XL drop time.
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#16
by
Jim
on 15 Mar, 2006 12:16
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#17
by
DaveS
on 15 Mar, 2006 13:33
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Pegasus drop-4 minutes.
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#18
by
Chris Bergin
on 15 Mar, 2006 13:35
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Keep on it Dave. I've got no feed here, for some reason.
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#19
by
Jim
on 15 Mar, 2006 13:37
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Chris Bergin - 15/3/2006 8:35 AMKeep on it Dave. I've got no feed here, for some reason.
Are you on the countdown page?