Reentry Data
Row Num,Name,Parent,Qty,Material,Body Type,Thermal Mass,Diameter/Width,Length,Height,Status,Risk,Demise Alt,Total DCA,KE
1,DPI LTM CubeSat,0,1,Aluminum 5052,Box,1.261,0.108,0.1135,0.108,,,,,
2,Primary structure (PROVES 1U frame),1,1,Aluminum 5052,Box,0.092,0.1,0.1135,0.1,,,,,
3,Flight controller (FC V5d LTM),1,1,Fiberglass,Flat Plate,0.0446,0.09,0.09,,,,,,
4,Battery pack board (battery_pack_v2),1,1,Fiberglass,Flat Plate,0.0446,0.09,0.09,,,,,,
5,Li-ion 18650 cells (2S2P),1,4,Steel AISI 316,Cylinder,0.046,0.018,0.065,,,,,,
6,AMSAT LTM (3-board PC-104 stack),1,1,Fiberglass,Box,0.13,0.092,0.09,0.033,,,,,
7,LTM harness (J30 to H1/H2),1,1,Copper Alloy,Box,0.01,0.02,0.05,0.005,,,,,
8,Solar panels (XY_Faces_V2a / Z),1,5,Fiberglass,Flat Plate,0.0025,0.07,0.09,,,,,,
9,Solar cells (KXOB101K08TF),1,30,Fiberglass,Flat Plate,0.0033,0.018,0.042,,,,,,
10,Antenna top cap (v2c),1,1,Fiberglass,Flat Plate,0.0427,0.1,0.1,,,,,,
11,Tape-measure antenna elements,1,2,Steel AISI 316,Flat Plate,0.0001,0.0127,0.1778,,,,,,
12,Card brackets,1,6,Aluminum 5052,Flat Plate,0.0044,0.02,0.088,,,,,,
13,L-brackets,1,4,Aluminum 5052,Flat Plate,0.0024,0.018,0.035,,,,,,
14,Feet (PA-12),1,8,Polyamide,Box,0.0021,0.014,0.031,0.007,,,,,
15,M2.5 fasteners,1,44,Steel AISI 316,Cylinder,0.0003,0.00238,0.01,,,,,,
16,M2.5 bolts + locknuts,1,16,Steel AISI 316,Cylinder,0.001,0.004,0.01,,,,,,
17,Wire harnessing,1,1,Copper Alloy,Box,0.17,0.028,0.028,0.028,,,,,
18,Torque rod cores,1,1,Iron,Cylinder,0.081,0.0127,0.07,,,,,,
19,Torque rod windings,1,2,Copper Alloy,Cylinder,0.004,0.005,0.07,,,,,,
20,Magnetorquer air coil,1,1,Copper Alloy,Box,0.2,0.02,0.0695,0.016,,,,,