STAGE 1 GEOMETRIC CHARACTERISTICS: FUSELAGE: TOTAL LENGTH (FT) STAGE DIAMETER (FT) LENGTH. Ii IAMETER RAT I0 AFT SKIRT LENGTH (FT) INTERTANK SPACING (FT) NOSE LENGTH (FT) LOX TANK LENGTH (FT) FUEL TANK LENGTH (FT) TOTAL TANK VOLUME INCL ULLAGE LOX TANK VOLUME FUEL TANK VOLUME WING: WING AREA (SQ FT) WING LOADING (LBS/SQ FT) WING SPAN (FT) STRUCTURAL WING SPAN (FT) ROOT CHORD (FT) THEORETICAL ROOT THICKNESS (FT) TIP CHORD (FT) TAPER RATIO ASPECT RATIO SWEEP OF FILLET (DEG) LEADING EDGE SWEEP (DEG) TRAILING EDGE SWEEP (DEG) SPANWISE DISTANCE DY 1 DYE CF Cl CE C3 C4 C5 Ct. C7 C8 (LAM C-E)l (LAM C--E)E CDS LAM 0'1 CDS LAM OE CDS LAM E EFF CLA TRUE CLA REF VERTICAL TAIL: VERTICAL TAIL AREA (SQ FT) HORIZONTAL STABILIZER: HORIZONTAL STABILIZER AREA (SQ FT?' TABLE VI-B-3-18
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