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1.00 for baseline ADOC aerodynamic aircraft airframe weight fraction Baseline BGT Definition baseline definition Baseline Value baseline vehicle BGT baseline buckling criteria c/ton-mile crippling criteria depreciable design factor designed by buckling designed by crippling designed by primary designed by stiffness designed by yield DOC elements DOC formulas DOCp Driver Parameters Driver Partial equations elevons empennage F design factor for fuselage factor for wing fuel fuselage structure designed GLOW GLOW GLOW gross lift-off weight hypersonic induced drag factor input data kg lb Lift-to-Drag Ratio LTPS M/TPS Method Module operating cost OUTPUT FROM MODULE payload compartment primary loads procedures Project Office propulsion Reference TABLE reinforced carbon-carbon Root chord specific impulse stiffness criteria structure not designed subsonic summary surface Table 4-IV TECHNOLOGY PARAMETER EQUATIONS TECHNOLOGY PARAMETER PARTIALS Technology Projections thermal protection system ton-mile turbojet turbojet engines W/A)Tps wing structure designed WpL/GLOW yield criteria zero-lift drag coefficient