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DESIGN AND DEFINITION OF PERFORMANCE POTENTIAL
Vehicle Design Analysis
2 other sections not shown
addition Advanced Earth Orbital advanced technology programs aerial refuel aerodynamic air launch aircraft airframe analysis ascent associated body frame Boeing Boundary layer transition brazed Bubble memories cost per flight cryogenic cycle costs DDT&E discounted dollars Earth Orbital Transportation estimate facility figure of merit GROUND ACCELERATOR hardware hydraulics hypersonic IDLE MODE OPERATIONS impact included inert weight inflight fueled l0 kg l976 dollars landing gear linear engine lower surface main engine main propulsion MAX g's MAX Q million dollars MISSION PROFILE mixture ratio NASA NORMAL TECHNOLOGY GROWTH operations costs Orbital Transportation Systems overall payload planform potential propulsion system Reduced system weight reentry result Rocketdyne Single Stage Slush/triple point Space Shuttle Space Shuttle program SSME SSTO vehicle Stage to Orbit SUMMARY SUPERSONIC TRANSPORT tank tankage tanker Task technology areas temperature thermal trajectory vehicle design vehicle GLOW vehicle system WEIGHT REDUCTION weight savings zero NPSH pumps