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keywords:(Nozzle Design)
Investigations of Thrust Vector Control for High-alpha Pitchover
Engine System Loads Development for the Fastrac 60K Flight Engine
Evaluation of a Platform Vertical Single-Component Thrust Stand
Marshall Space Flight Center Surface Modeling and Grid Generation Applications
Research Achievements Review, Volume 4, No. 6 Chemical Propulsion Research at Msfc
Study of Aerodynamic Technology for Single-Cruise Engine V/STOL Fighter/Attack Aircraft
Design and Analysis of Axial Turbine Using Three Different Vortex Laws
Mars Sample Return Mars Ascent Vehicle Mission and Technology Requirements
Development of the Subliming Solid Control Rocket, Phase II
Control System for the X-33 Linear Aerospike Engine
Space Shuttle Orbit Maneuvering Engine Reusable Thrust Chamber
Development of Low Cost Ablative Nozzles for Large Solid Propellant Rocket Motors
Space Storable Engine Characterization Final Report