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  Space Shuttles - Space Station
  ISS assembly order: truss vs. modules

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Author Topic:   ISS assembly order: truss vs. modules
NavySpaceFan
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Posts: 655
From: Norfolk, VA
Registered: May 2007

posted 09-17-2007 11:46 AM     Click Here to See the Profile for NavySpaceFan   Click Here to Email NavySpaceFan     Edit/Delete Message   Reply w/Quote
Judging by the mission number of its assigned flight, the mission to deliver and install the S-6 truss/arrays should be the next to launch. However, the next few assembly flights deliver four new node/laboratory modules. Why the change? Was there political considerations in getting the ESA/JAXA modules up sooner? Is it due to some problem with the S-6 truss? Is it a crew training issue? Thanks!

cspg
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Posts: 6210
From: Geneva, Switzerland
Registered: May 2006

posted 09-17-2007 11:46 AM     Click Here to See the Profile for cspg   Click Here to Email cspg     Edit/Delete Message   Reply w/Quote
Apparently there's enough power on the Station to power the new modules, which will increase the man-rated capability of the station to a 6-person crew. Before adding even more power, maybe the reasoning is that they want to check all electrical connections first to see if everything is ok. Also no new modules were added since 2001 and I'm wondering if there's a ground storage issue (easier to store a truss than a pressurized module?).

Chris.

Jay Chladek
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Posts: 2272
From: Bellevue, NE, USA
Registered: Aug 2007

posted 09-18-2007 01:27 AM     Click Here to See the Profile for Jay Chladek   Click Here to Email Jay Chladek     Edit/Delete Message   Reply w/Quote
Another thing to consider is they are probably also wanting to start doing more science experiments then what the Destiny module can accomplish. As such, the ESA and JAXA modules will potentially allow them to do that. A solar array on the otherhand just produces power and with the second main array up and working, they have power to spare now. The main reason I imagine that they wanted to get the two arrays on the main truss in quick fashion probably has to do with the sail drag of one array on the structure. By getting a symetrical configuration to the ISS, I figure there weren't as many issues with the station's gyro systems once they got the arrays to begin sun track rotations.

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