Nuclear Thermal Rocket Engine with a Toroidal Aerospike Nozzle [thesis]

Kyle Stewart
NUCLEAR THERMAL ROCKET ENGINE WITH A TOROIDAL AEROSPIKE NOZZLE by Kyle J. Stewart This thesis describes the coupling of a nuclear thermal rocket engine with a toroidal aerospike nozzle. The coupling of the two systems consists of two phases. The first of these phases begin with top-level systems and subsystems analysis and design of the new engine. The second phase is the analysis and characterization of the major engine systems
doi:10.31979/etd.qwkv-999v fatcat:tpnimnhwa5agllj7vz362hdnq4