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Structures and Materials Orlando
Flight Control W K Waymeyer and R W Sporing
Launch Vehicle Control
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acceleration alloys aluminum antenna atmosphere axial batteries bending beryllium block diagram Bode plot Brayton cycle cabin carbon chamber chemical components condensing control system crew density duration dynamic effects efficiency electrical electrolyte electrons elements energy engine equation factor flight flow fluid flux force frequency fuel cell gases heat exchanger heat rejection hydrogen increase input ionization isotope launch vehicle limit liquid propellant loads loop material maximum mercury meteoroid micrometeoroid mission mode monocoque neutron nonlinear nozzle nuclear operating orbit output oxidizer oxygen parameters phase power system pressure propellant rocket propulsion system psia radiation Rankine cycle ratio reaction reactor Regenerative Heat Exchanger result root locus rotation Sabatier reaction shown in Figure solar cells solid propellant space vehicle spacecraft specific impulse stage storage stress structure subsystems tank techniques temperature thermal thermoelectric thrust tion titanium turbine typical valve vapor velocity voltage weight welded zero