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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
Software Infrastructure for an Autonomous Ground Vehicle
Launch Vehicle Health Management
Parametric Modeling and Simulation for Aerodynamic Design of Launch Vehicle
An Open Integrated Electronic System Software Architecture Design for Launch Vehicle