A Systems Design for a Prototype Space Colony

6.58 FIGURE 6.24: POWER FLOW VERSUS THERMAL CONDUCTIVITY OF SHIELD 4.0 ,------------------- Q) (J rtJ 3 .0 o. 2. 0 Cl) 0 +I +I ::, 0. +I 6 1.0 H ~ R. Glass 0 .___..__.____.___.___ L.......L.......1-...L......J .1 . 5 1 5 10 50 100 Thermal Conductivity of Shield (watts/m-°K) 500 1000

RkJQdWJsaXNoZXIy MTU5NjU0Mg==