1. Subsystem-First Engineering
The SPX is treated as a modular propulsion architecture. Each major subsystem is defined, reviewed, improved, and validated before complete module integration.
Hilgart Aerospace programs are focused on the Kratos SPX modular sub-system architecture. Each major subsystem is presented as an individual engineering track designed for review, refinement, validation, and future integration into the complete propulsion module.
Primary propulsion architecture built around defined subsystem interfaces.
Each subsystem is evaluated before full integration into the propulsion module.
University, technical advisor, and laboratory review may support each track.
Current focus is engineering package refinement and subsystem validation planning.
The programs page is centered on the six major SPX subsystem tracks.
The SPX is treated as a modular propulsion architecture. Each major subsystem is defined, reviewed, improved, and validated before complete module integration.
The first validation priority is the balance between power generation, waste heat production, coolant transport, heat rejection, material limits, and auxiliary recovery.
The programs page now emphasizes engineering discipline, risk reduction, and validation.
Hilgart Aerospace approaches program development through disciplined systems engineering: define the subsystem, identify the assumptions, challenge the assumptions, validate the data, and then integrate only after the technical foundation is strong enough to support the complete architecture. This structure is intended to reduce technical risk, improve serviceability, and preserve design flexibility as the SPX evolves.
A subsystem-based program structure allows investors, universities, advisors, and technical partners to evaluate specific engineering problems instead of being asked to assess an entire propulsion platform at once.
Devotion, Positive Environment, Critique, Honesty, Flexibility, Focus, Dedication, Persistence, Perseverance, Belief, Understanding, be Team Orientated, Imagination, Trust, Creativity and Respectful. Without all of these, it isn’t worth the effort. -KTH
First validation priority focused on thermal-power balance, heat rejection, coolant selection, radiator sizing, thermal spine design, material limits, and subsystem reliability.
Supporting subsystem focused on waste heat recovery, auxiliary power generation, power conditioning, and integration between the thermal management system and onboard loads.
Propulsion subsystem focused on controlled chemical-plasma interaction, multi-gas flow management, combustion stability, plasma conditioning, and safe operating envelopes.
Subsystem track focused on magnetic-field interaction, plasma flow stabilization, propellant behavior, throat control, and performance consistency through the engine core.
Subsystem track focused on exhaust shaping, plume stabilization, nozzle expansion behavior, vector-control concepts, thermal exposure, and downstream mission-control effects.
Control architecture focused on monitoring, diagnostics, fault response, subsystem coordination, data processing, autonomous assistance, and long-term adaptive operation.
The SPX roadmap is structured around focused subsystem milestones. Each subsystem is intended to move through definition, review, modeling, trade studies, test planning, and validation before complete module integration.
Define interfaces, operating assumptions, performance boundaries, thermal limits, and validation questions.
Review models, drawings, materials, risk areas, failure points, and manufacturing assumptions.
Evaluate coolant media, materials, power balance, controls, interfaces, and alternate design paths.
Prepare test articles, instrumentation plans, university/laboratory review, and milestone funding requirements.