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Discover X-33 Reusable Launch Vehicle
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Reconfigurable flight control designs with application to the X-33 vehicle
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X-33 integrated test facility extended range simulation
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Reconfigurable control design for the full X-33 flight envelope
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Thermal management design for the X-33 lifting body
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The X-33 extended flight test range
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The revamping of an ignition test facility
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The control system for the X-33 linear aerospike engine
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Evaluation of microcracking in two carbon-fiber/epoxy-matrix composite cryogenic tanks
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A strategy for integrating a large finite element model using MSC NASTRAN/PATRAN
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The Reusable Launch Vehicle Technology Program and the X-33 advanced technology demonstrator
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X-33/RLV
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X-33/RLV
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X-33 phase II
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Development of the X-33 aerodynamic uncertainty model
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An inviscid computational study of an X-33 configuration at hypersonic speeds
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Design and calibration of the X-33 flush airdata sensing (FADS) system
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Analysis of aerospike plume induced base-heating environment
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