• Architecture approach to maximize mission capture

 • Multiple stage systems for near-term use

 • People and major cargo flown separately

 • Take advantage of existing assets

 • Kerosene fuel for boosters; external carry of liquid hydrogen

 • Winged recovery & wheeled runway landings (150 knots or less)

 • Heat sink thermal protection up to Mach 6

 • Glideback recovery from Mach 3; Flyback recovery from beyond Mach 3

• Operationally efficient design approaches

• Large design margins (e.g. 30% weight margin)

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