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Investigation of solid plume simulation criteria to produce flight plume effects on mulitbody configuration in wind tunnel tests
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NASA Glenn Research Center's hypersonic propulsion program
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Review of our national heritage of launch vehicles using aerodynamic surfaces and current use of these by other nations
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Trajectory optimization for an asymmetric launch vehicle
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Optimal guidance law develpment for an advanced launch system
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Rationales for the Lightning Flight-Commit Criteria
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Packaging, deployment, and on-orbit assembly options for large geostationary spacecraft
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Low Cost Large Core Vehicle Structures Assessment
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Affordable spacecraft
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Launch vehicle flight control augmentation using smart materials and advanced composites (CDDF project 93-05)
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RL10A-3-3A rocket engine modeling project
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High leverage space transportation system technologies for human exploration missions to the moon and beyond
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Cryogenic on-orbit liquid depot-storage, acquisition and transfer (COLD-SAT) experiment conceptual design and feasibility study
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Airborne rotary air separator study
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SEE design guide and requirements for electrical deadfacing
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Launch vehicle performance with solid particle feed systems for atomic propellants
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Design of launch vehicle flight control augmentors and resulting flight stability and control (Center Director's discretionary fund project 93-05, part III)
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Launch vehicle performance with solid particle feed systems for atomic propellants
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Electric propulsion options for a magnetospheric mapping mission
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Catalogue of X-ray texture data for Al-Cu-Li alloy 1460, 2090, 2096 and 2195 near-net-shape extrusions, sheet and plate
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Launch vehicle integration options for a large earth sciences geostationary platform concept
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Design and fabrication of the NASA HL-20 full scale research model
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Advanced transportation system study
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Applying Monte Carlo simulation to launch vehicle design and requirements analysis
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