Development of the K-1 two-stage, fully reusable launch vehicle
Development of the K-1 Two-Stage, Fully-Reusable Launch Vehicle
Results for a fully reusable TSTO-launch vehicle concept
Results for a Fully Reusable TSTO-Launch Vehicle Concept
Investigation of base flow on a space rocket with plumes
Investigation of Base Flow on a Space Rocket with Plumes
Development and capabilities of the NASA Langley Cryogenic Pressure Box
Development and Capabilities of the NASA Langley Cryogenic Pressure Box
Computational simulation of EM attenuation by plasmas formed in hypervelocity atmospheric flight
Computational Simulation of EM Attenuation by Plasmas Formed in Hypervelocity Atmospheric Flight
Progress in SSTO and TSTO aerospace plane combined propulsion system research program ('ORYOL-2-1')
Progress in SSTO and TSTO Aerospace Plane Combined Propulsion System Research Program ("ORYOL-2-1")
Computational study of hypervelocity impacts on metallic thermal protection systems
Computational Study of Hypervelocity Impacts on Metallic Thermal Protection Systems
Effects of melt layer on steady aerodynamic ablation in hypersonic flow
Effects of Melt Layer on Steady Aerodynamic Ablation in Hypersonic Flow