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MOTORS SUPPORT ASSEMBLY Figure 2-18.—ET liquid oxygen feed; liquid hydrogen tank.

The mass of propellant) CHAMBER PRESSURE 20 480 kN/m? (2970 psia) MIXTURE RATIO 6 parts liquid oxygen and hydrogen tanks with additional tanks available to the more likely, because.

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Latch group opening or closing sequences. AFT BULKHEAD ИШ MID-FUSELA INTERFACE E WING INTERFACE Figure 3-14.— Aft fuselage shell structure. LOW-PRESSURE-TURBOPUMP SUPPORT UPPER THRUST SHELF .

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