Can do on the assembly, and unless we rearrange the valves, 6" gives the least complex tubing arrangement. So all will be used. Chris Hayes Boston University Mechanical Engineering 2014 BU SEDS President BU AIAA Vice President NewSpace Policy Initiative Chair BU RPG Mechanical Designer cbhayes@xxxxxx 617-823-1536 On Oct 26, 2013 10:25 PM, "Armor Harris" <armorharris@xxxxxxxxx> wrote: > It's going to be that long, or is this extra stock for machining purposes? > > > On Sat, Oct 26, 2013 at 9:02 PM, Christopher Hayes <cbhayes@xxxxxx> wrote: > >> Hey Armor, just to let you know, the CAD for the shell is finalized. We >> need 1 6" section of the rocket tubing and 2 3" couplers. >> >> The files on drive are outdated, I wasn't able to put the new ones up. >> >> Chris Hayes >> >> Boston University >> Mechanical Engineering 2014 >> >> BU SEDS President >> BU AIAA Vice President >> NewSpace Policy Initiative Chair >> BU RPG Mechanical Designer >> >> cbhayes@xxxxxx >> 617-823-1536 >> On Oct 26, 2013 8:52 PM, "D. Armor Harris" <davidh@xxxxxx> wrote: >> >>> Hey Everyone, >>> >>> We'll be meeting in the wind tunnel lab on Monday (Room 113 of 110 >>> Cummington St) at 7pm. See you all there! >>> >>> Also for anyone doing CAD work, there are some templates that you should >>> use so everyone's drawings look equally professional and have the right >>> tolerances. They're in >>> >>> \Google Drive\BURPG\Reference\CAD Standards along with installation >>> instructions. >>> >>> >>> -- >>> David Armor Harris >>> Boston University Rocket Propulsion Group >>> davidh@xxxxxx >>> >> >