EFFECT OF THE WIDTH AND NUMBER OF RINGS OF CONCENTRIC SPLIT RING RESONATOR ON PLASMA GENERATION FOR MINIATURE ION THRUSTER

von Nagarajan, Nageshwar
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Electric propulsion (2021)

MAGNETIC DEFLECTION OF A LOW-TEMPERATURE PLASMA JET FOR A MAGNETIC NOZZLE FOR PULSED FISSION-FUSION ENGINE

von White, Zachary
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Nuclear and future flight propulsion (2021)

DEVELOPMENT OF AN OPTICALLY ACCESSIBLE RACETRACK-TYPE ROTATING DETONATION ROCKET ENGINE

von Unruh, Evan C.
Veröffentlicht in AIAA Propulsion and Energy Forum (2020 : Online) Pressure gain combustion (2020)

EXPERIMENTAL STUDY OF A RACETRACK-TYPE ROTATING DETONATION ROCKET ENGINE WITH SHEAR-COAXIAL INJECTORS RUN ON GASEOUS METHANE AND OXYGEN

von Unruh, Evan C.
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Pressure gain combustion (2021)

Mixing and Recovery Performance of Triplet Impinging Injectors with Varying Flow Areas for Detonative Combustion

von Hemming, Michaela R.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Pressure gain combustion (2023)