The selected candidate will perform modeling, simulation, and data analysis in support of selecting potential landing sites on the Moon for the Artemis III, IV, and V, missions as well as other relevant lunar missions being planned by industry partners. Selection of the optimal landing sites for the first crewed mission of the Human Landing System (HLS) will involve compl

The selected candidate will perform modeling, simulation, and data analysis in support of selecting potential landing sites on the Moon for the Artemis III, IV, and V, missions as well as other relevant lunar missions being planned by industry partners. Selection of the optimal landing sites for the first crewed mission of the Human Landing System (HLS) will involve compl

The selected candidate will support the growth, refinement, and improvement of the NASA Glenn developed software package, GRC Communication Analysis Suite (GCAS), that is used for the analyses of selecting potential landing sites on the Moon for the Artemis III, IV, and V, missions as well as other relevant lunar missions being planned by industry partners. GCAS was devel

The selected candidate will support the growth, refinement, and improvement of the NASA Glenn developed software package, GRC Communication Analysis Suite (GCAS), that is used for the analyses of selecting potential landing sites on the Moon for the Artemis III, IV, and V, missions as well as other relevant lunar missions being planned by industry partners. GCAS was devel

The selected candidate will support the Human Lander System (HLS) Site Availability team in the distribution of results by exporting all site data and associated information in a variety of formats as defined and needed by the multiple customers of the analyses. The NASA Glenn developed software package, GRC Communication Analysis Suite (GCAS) is used for the analyses of

The selected candidate should have experience in the aerodynamic analysis, design, and airframe integration of aircraft engine inlet and exhaust nozzle systems. Job responsibilities will include Generating innovative conceptual aerodynamic designs of installed aircraft exhaust nozzles for improved performance and reduced acoustic emissions. Performing Computational Fluid