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|    sci.space.policy    |    Discussions about space policy    |    106,651 messages    |
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|    Message 105,880 of 106,651    |
|    Greg (Strider) Moore to JF Mezei    |
|    Re: Testing of quick disconnects    |
|    30 Sep 22 13:19:44    |
      From: mooregr@deletethisgreenms.com              "JF Mezei" wrote in message news:74qYK.341737$wLZ8.104544@fx18.iad...       >       >On 2022-09-26 08:34, David Spain wrote:       >       >> As Rand Simberg points out on his blog a whole set of clocks start       >> ticking once the SLS rocket rolls out of the VAB.       >       >I can understand SRBs which have a "best before" date because       >built-already fueled. I can understand limits on how many times you       >can fill/empty the tanks since going from tropical to cryo temperature       >cycles impacts the metals.       >       >But to design the Orion Capsule such that it either doesn't get power       >from pad or didn't bother with provisions to power experiments while at       >pad is very strange for NASA. Same with the flight termination system       >whose batteries should be able to be recharged while at pad.              Two schools of thought on something like that:       1) If we're launching only once or twice a year, why develop all the       infrastructure at the pad?       2) On the other hand, because we plan on only launching once or twice a       year, it could be we're at the pad for long periods of time, so we should       develop the need for it.              Think of it this way too. For a variety of reasons Apple started the trend       of not being able to quickly/easily swap out batteries on their iPhones. For       one, it makes it lighter. Fewer connections, etc. For another, "well folks       will upgrade before the battery dies..."              Also, rechargeable batteries are a bit more complicated, adds weight,       potential outgassing, potential over charging, etc. So you can argue it       might be safer to do all that work in a separate building, not on the rocket       itsefl.                            >       >The odds of delays at pad are the same whether rocket is reusable or       >not. And the cost of providing pad power to these systems wouldn't be       >that great compared to overall cost.       >       >It is just strange that pedantic NASA wouldn't have required the rocket       >to be able to stand at pad without using batteries.       >       >> continue on the Shuttle even after it had been rolled out to the pad.       >> SLS does not have this, because why would you need to service an       >> *expendable* rocket?       >       >       >It was decided to complete preparation at the pad, and load payloads at       >the pad, hence the RSS for shuttle. But the shuttle itself was getting       >pad power and the crew compartment was fully powered and experiments,       >fridges etc powered by pad until a minute or two before launch.       >       >The fact that SLS can't be maintained at pad is all the more reason to       >allow it to be powered by the pad since changing AA or CR2032 batteries       >spread throughout the stack requires roll back to the VAB.              I would tend to agree. Shuttle, for all its problems WAS in theory designed       for quick servicing, which meant being able to do a good deal of work at the       pad.       SLS obviously wasn't.              Heck, even the Saturn V had the mobile service structure!              --       Greg D. Moore http://greenmountainsoftware.wordpress.com/       CEO QuiCR: Quick, Crowdsourced Responses. http://www.quicr.net       IT Disaster Response -       https://www.amazon.com/Disaster-Response-Lessons-Learned-Field/dp/1484221834/              --- SoupGate-Win32 v1.05        * Origin: you cannot sedate... all the things you hate (1:229/2)    |
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