An Extremely High Isp Spacecraft Propulsion System
Preliminary Analysis of the Gradient Field Imploding Liner Fusion Propulsion Concept
Preliminary Analysis of the Gradient Field Imploding Liner Fusion Propulsion Concept
Ignition and Burn in a Hybrid Nuclear Fuel for a Pulsed Rocket Engine
NASA-NIAC 2001 Phase I Research Grant on Aneutronic Fusion Spacecraft Architecture