Quote from: corrodedNut on 05/22/2012 09:25 amQuote from: sojourner on 05/22/2012 09:24 amCan someone tell me why the solar panels on Dragon look white in those images? It doesn't appear to be caused by the lighting/angle.BacksideAh, didn't realize they were one sided. silly me.
Quote from: sojourner on 05/22/2012 09:24 amCan someone tell me why the solar panels on Dragon look white in those images? It doesn't appear to be caused by the lighting/angle.Backside
Can someone tell me why the solar panels on Dragon look white in those images? It doesn't appear to be caused by the lighting/angle.
Do they have to be one-sided? Can future versions maybe have both sides being photovoltaic, for more power? Or is that impractical?
Quote from: MP99 on 05/20/2012 10:25 am1) Is it likely the mixture-adjustment hardware could compensate for a LOX-rich bias in an engine, at least to carry it through the first seconds of flight until the point where the Falcon can struggle on with eight engines? I'm guessing not, as I assume the actual adjustment range would be quite small.2) Also, how does the stage determine the remaining prop levels - does it just integrate the flow levels? If so, would the flow be measured per-engine or before the octopus? If flow is measured per-engine, I guess that would be a useful indication to the engine controller of a problem.1) Hard to say. If there's closed-loop engine control, maybe. Too many branches of the fault tree to say for sure. Not sure it's even desirable to try and fly through it. Abort may be the better choice.2) Tank bottom pressure. Flight computer solves for h in P_b = P_ull + rho*g*h. There are patents on it that are available with a web search.
1) Is it likely the mixture-adjustment hardware could compensate for a LOX-rich bias in an engine, at least to carry it through the first seconds of flight until the point where the Falcon can struggle on with eight engines? I'm guessing not, as I assume the actual adjustment range would be quite small.2) Also, how does the stage determine the remaining prop levels - does it just integrate the flow levels? If so, would the flow be measured per-engine or before the octopus? If flow is measured per-engine, I guess that would be a useful indication to the engine controller of a problem.
Silly question, does Dragon use Ku-band or only S-band? Think it is the latter.
Dragon can also communicate on S-band viaeither tracking and data relay system(TDRSS)or ground stations.
I didn't get to see it live, does anyone have a video link to the post launch press conference? I found Bolden's comments, but can't find the full press conference.Bolden's speech is here: http://www.youtube.com/user/SpaceRefOnOrbit
After mvac ignition there is seems o be a fluid coming from above the nozzle, is this just melting ice as it is a significant amount at first then tapers down to only occasional drops?
AirmanPika,Nice pic - It looks like a more significant payload processing area extension than I thought. The added height - perhaps they want to be able to do vertical payload processing, at least for the payload and fairing?
Quote from: Lars_J on 05/22/2012 05:55 amAirmanPika,Nice pic - It looks like a more significant payload processing area extension than I thought. The added height - perhaps they want to be able to do vertical payload processing, at least for the payload and fairing?Just vertical encapsulated payload receiving and breakover. Payload might still be processed at another facility.
Quote from: carrotSnack on 05/22/2012 09:32 amQuote from: Bogeyman on 05/22/2012 09:28 amIs there any map or something where one can see where Dragon is right now? Maybe this http://www.n2yo.com/?s=77777 ?Dragon chasing ISS:-http://www.n2yo.com/?s=25544|77777cheers, Martin
Quote from: Bogeyman on 05/22/2012 09:28 amIs there any map or something where one can see where Dragon is right now? Maybe this http://www.n2yo.com/?s=77777 ?
Is there any map or something where one can see where Dragon is right now?
This is a pleasant surprise, I didn't think that SpaceX would get this far this year.