Nice thing about recovering the rocket stage is you ALSO can recover the helium that's pressurizing it. The helium fills the ullage volume, it's not expended!
Quote from: Robotbeat on 01/05/2016 06:03 pmNice thing about recovering the rocket stage is you ALSO can recover the helium that's pressurizing it. The helium fills the ullage volume, it's not expended!Yes, but it looks like the remaining LOX is vented after landing, so that would also vent the helium.
You do know every other launcher expends the helium if it's used to pressurize nice to even be discussing reuse of helium from the copv bottles
Quote from: avollhar on 01/05/2016 08:22 amQuote from: cscott on 01/05/2016 07:39 amAt the time this was explained as needing to have a constant thermal emissivity so that IR imaging could obtain correct temperatures for every surface point. Otherwise you have to calibrate for the emissivity of every different surface separately.I don't think it's related to soot.With the right paint (higher IR emissivity), you can effectively cool via radiation. One reason why electronic heatsinks are black anodized rather than polished aluminum.If your semiconductor heatsink is cooling appreciably via radiation compared to convection then youare having a very bad day.Most heavy duty heatsinks I see are strip or extruded aluminum, albeit matte rather than polished.
Quote from: cscott on 01/05/2016 07:39 amAt the time this was explained as needing to have a constant thermal emissivity so that IR imaging could obtain correct temperatures for every surface point. Otherwise you have to calibrate for the emissivity of every different surface separately.I don't think it's related to soot.With the right paint (higher IR emissivity), you can effectively cool via radiation. One reason why electronic heatsinks are black anodized rather than polished aluminum.
At the time this was explained as needing to have a constant thermal emissivity so that IR imaging could obtain correct temperatures for every surface point. Otherwise you have to calibrate for the emissivity of every different surface separately.I don't think it's related to soot.
In this forum I am obviously talking about near-space/vacuum conditions. And then surface coating makes a huge difference as you are purely radiative. The emissivity for aluminum varies from 0.05 (polished) over 0.21(sandblasted) to 0.77 (anodized) (source http://www.infrared-thermography.com/material.htm) which does make a difference in vacuum.That said, the Merlin engine bell is made from some niobium alloy and the game might change.
No. You've thinking of venting the gas above the LOX which is a mix of oxygen and helium. If you were to do that you'd still have nearly all of the LOX and would have to wait for it to boil into gas then vent that gas, a long process. What needs to happen is to vent the LOX from the bottom of the tank and stop that venting process once the liquid is out of the tank. ...Which leaves all of the helium in the tank for re-use (after cleaning it up). And don't forget about the He on top of the fuel as well.
Quote from: toruonu on 01/05/2016 06:42 pmYou do know every other launcher expends the helium if it's used to pressurize nice to even be discussing reuse of helium from the copv bottles Yes, but the others don't have the goal / vision / ambition of daily launches to consider.
The removal ops would not fit in with Spacex turnaround times, since it would be time consuming. Just remove the RP-1 and open the all the vents.Spacex is just going vent the He. Quicker and cheaper.
1. They're not known for leaving a penny on the ground. 2. They did send back all the lox to the gas plant when the COPV blew on the 1st Orbcomm launch and I think it's worth about the same.
Funny. But.It belongs in a lab, in pieces, to expedite searching for any close-calls or low-margin situations with the rocket. Destructive testing as well.…
Quote from: meekGee on 01/05/2016 04:18 pmFunny. But.It belongs in a lab, in pieces, to expedite searching for any close-calls or low-margin situations with the rocket. Destructive testing as well.…One question I have about all this expectation of tear-downs and forensic examinations is how much it will cost? The manpower and time for what may prove a fruitless search might be a good reason not to do it.The better plan could be 'test as you fly' i.e. after checking for gross damage they do a static fire. It is a procedure they do a lot, does not require special expertise, tests engines and structure, and errors will be easily apparent.Keeping the first stage returned for posterity is pretty sentimental but if that is the price for having a visionary CEO who has got the company this far and could take them much further then we should be willing to bare it.
Quote from: chalz on 01/05/2016 11:28 pmQuote from: meekGee on 01/05/2016 04:18 pmFunny. But.It belongs in a lab, in pieces, to expedite searching for any close-calls or low-margin situations with the rocket. Destructive testing as well.…One question I have about all this expectation of tear-downs and forensic examinations is how much it will cost? The manpower and time for what may prove a fruitless search might be a good reason not to do it.The better plan could be 'test as you fly' i.e. after checking for gross damage they do a static fire. It is a procedure they do a lot, does not require special expertise, tests engines and structure, and errors will be easily apparent.Keeping the first stage returned for posterity is pretty sentimental but if that is the price for having a visionary CEO who has got the company this far and could take them much further then we should be willing to bare it.I agree. Test that which has flown then refly. Visual and non destructive will get you down the road. It's not like they intend to fly to exhaustion.Regarding saving the first stage. It is serving a required function at 39A. Further if one needs to be dissected like an alien in a SciFi movie than surely waiting 2 months from Orbcomm to SES-9 or CRS-8 shouldn't be too much to ask. Also, the eyes of history doesn't care much about 2nd.59 years after Sputnik what's another month or two? 🤔Edit: remove cheekiness
Quote from: saliva_sweet on 01/05/2016 08:18 pm1. They're not known for leaving a penny on the ground. 2. They did send back all the lox to the gas plant when the COPV blew on the 1st Orbcomm launch and I think it's worth about the same. 1. Yes they are. They run into a lot of dead ends.2. what LOX?
Quote from: Jim on 01/05/2016 08:39 pmQuote from: saliva_sweet on 01/05/2016 08:18 pm1. They're not known for leaving a penny on the ground. 2. They did send back all the lox to the gas plant when the COPV blew on the 1st Orbcomm launch and I think it's worth about the same. 1. Yes they are. They run into a lot of dead ends.2. what LOX?1) That was just my impression given they're happy to go dumpster diving to get the stuff they like for cheap.2) When they were prepping for OG2-1 launch a COPV blew. The launch was delayed by more than a month so they had a bunch of lox left over. They shipped it back in trucks. I may recall incorrectly.
Quote from: meekGee on 01/05/2016 04:18 pmFunny. But.It belongs in a lab, in pieces, to expedite searching for any close-calls or low-margin situations with the rocket. Destructive testing as well.…One question I have about all this expectation of tear-downs and forensic examinations is how much it will cost? The manpower and time for what may prove a fruitless search might be a good reason not to do it.