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CHAPTER PAGE 1 HISTORICAL PREFACE
SIZING THE VEHICLE
6 other sections not shown
absorptance alloy aluminum antenna approximately axial beam bearing beryllium beryllium copper booster boundary lubrication buckling coefficient circuit components compression conduction configuration convection critical curve cylinder deformation devices double corrugation dynamic effects efficiency elastic electrical electronic emittance energy engineer epoxy equation example expression extremely factor failure flight fluid friction function gear geometry heat transfer input integrated circuits interconnected Jet Propulsion Laboratory JPL photograph launch load lubrication material maximum meteoroid modes modules molybdenum disulfide monocoque motion nondimensional normal obtained operating packaging packaging engineer panels parameter planet plate portion pressure problems Propulsion radiation ratio reflected resonance rolling-element bearing sandwich shearing stress shown in figure shows simulator single corrugation solar solar constant solution space spacecraft structure spherical caps static steel strength subassemblies surface techniques temperature control theory thermal thickness tion titanium torque tube tube vacuum values various vehicle velocity vibration weight welded