Propulsion Systems Analyses

Propulsion Systems Center

The Propulsion Systems Center has the extensive analysis experience, capabilities and tools needed to design propulsion systems, high-energy lasers and cryogenic coolers.

Combustor Performance

Analyses include the effects of non-equilibrium chemistry and multiple phases. A detailed combustor analysis (3-dimensional, non-equilibrium chemistry) to evaluate heat transfer and combustion efficiency was central to the design of Northrop Grumman's advanced SCAT thruster.


Plume Effects

Plume effects analysis capabilities include evaluating high altitude plume effects (plume impingement and contamination) and plume signatures (IR, VUV and millimeter wave) using direct simulation Monte Carlo simulation. Plume signature analyses incorporate proprietary methods for all types of thrusters over a wide span of wavelengths.

Propellant Management and Slosh Effects

Propellant management device and propellant slosh characterization capabilities range from micro-gravity to launch environments. Several detailed computational fluid dynamics (CFD) tools support these design efforts.

Structural, Dynamics, Heat Transfer

Design analysis of propulsion, HEL, and cryogenic-cooler system components using commercial software tools (e.g., ANSYS).