BS PD CEN/CLC/TR 17603-31-03:2021 PDF
Factors affecting the equilibrium temperature of a spacecraft surface are described in this Part 3 using simple geometrical configurations and basic assumptions.
Methods for conducting calculations on the affect of Solar, planetary and albedo radiation are given taking into consideration the internal and immediate environmental factors and incorporating the various configurations and dimensions of the constituent parts.
More Standards PDF
SAE AMS4152M
$28.00 $56.00
SAE J470_201802
$55.00 $111.00
SAE AS9465B
$24.00 $49.00
SAE 9990/1
$43.00 $87.00









