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Saturn in-Flight Experimental Payload Study. Mid-Term Progress Report
Saturn in-Flight Experimental Payload Study. Volume I - Summary
Review of EMC practice for launch vehicle systems
A fault-tolerant architecture for launch vehicle guidance and control. I. Requirement/architecture
System architecture for Byzantine resilient computation in launch vehicle applications
A fault-tolerant architecture for launch vehicle guidance and control. II. Implementation
Dynamic test bed for the on-board computer system of a space launch vehicle
A flexible fault tolerant processor for launch vehicle avionics systems
Materials characterization and joint testing on the X-34 reusable launch vehicle
High temperature polyimide foams for aerospace vehicles
Carbon aerogel thermal protection system for reusable launch vehicles
A high assurance on-line recover technology for a space on-board computer
High temperature polyimide materials in extreme temperature environments
Ceramic matrix composite material in highly loaded journal bearings
Benefits of surface coatings for impacted composites to be used for cryogenic tankage
Reentry flight and ground testing experience with hot structures of C/C-SiC material
Role of Flight Experiments in the Development of Cryogenic Fluid Management Technologies
Software Infrastructure for an Autonomous Ground Vehicle
Footprint calculation for a reusable launch vehicle based on dynamics programming
Launch Vehicle Health Management
Parametric Modeling and Simulation for Aerodynamic Design of Launch Vehicle
Potential Composite Structures for NASA Future Launch Vehicles and Crew Spacecraft
The very specific vortex shedding test on vega launch vehicle
Effect of insulation layer for thermal shock in cryogenic composite laminates
An Open Integrated Electronic System Software Architecture Design for Launch Vehicle
PCE-Based Robust Trajectory Optimization of Launch Vehicles via Adaptive Sample and Truncation