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absorptance and emittance aircraft and spacecraft aluminum and graphite/epoxy aluminum structures baseline aluminum design compos composite materials conducted cosmic radiation CTE values data from ref Definition and Preliminary definition phase diameter dosage electromagnetic radiation evaluate fiber Figure Fireworthiness fracture ft/sec GLASS TRANSITION TEMPERATURES GRAPHITE/EPOXY Material graphite/epoxy structure interlaminar shear strength internal damage ionization isogrid structure Johnson Space Center km/s Langley Research Center LEO environment low Earth orbit low-velocity impact manufacturing techniques material loss material selection process mechanical considerations ment microcracks NASA Langley Research NASA Space Station NORAD outgassing pressure shells private communication radiation consists Research Center Hampton ring frames Room temperature September 15 single-skin Skylab space debris space environment Space Shuttle orbiter Space Station Definition Space Station structure Specific stiffness specific strength Station structural design stiffened structural material issues thermal conductivity thermal considerations thermal control thermal cycling thermal fatigue tion tubes ture vacuum values for graphite/epoxy velocities weight