LSM Public Document

System                Mass(kg)        Power(W)                    Volume (m^3)
 * Thermal Info Required/Collaboration between groups
 * Structures temperature requirements
 * Confirm that the Structures group is responsible for considering the effects of thermal cycling on the materials. 

Landing Gear        500                100 max (20 typical)        0.5

Docking                350                70 max (20 typical)           0.5

Hull Structure        15500            -                                25 (enclosed)

Mechanisms            50               100 max                         0.1

mechanisms is entirely guessed at.

What  Bowden said:

Link for Conical Shell Equations
 * need margin of safety table w/ every piece of primary structure (essential for the mission eg thrust structure landing gear pressure hull, deployment mechanisms) ex. landing leg -- landing impact load, landing impact stress, SF,
 * 1.5 to yield, 2.5 to ultimate (all positive)
 * calc MoS
 * for more complicated components, make a FEA model
 * For Rasc-al, use 3D printer, maybe make an animation
 * do the numbers for all the trade studies even if we don't think they'll work
 * pick a number out of thin air for the analysis so we can start the analysis
 * hand out tasks at the beginning of the meeting

http://www.isogrid-sst.com/Scan%20to%20PDF/sp8019.pdf