Vision remains important. Validation comes first.
Thermal Management Validation
The first engineering priority is proving the balance between power input, waste heat generation, coolant transport, heat rejection, radiator capacity, material limits, and auxiliary power recovery.
Subsystem Interface Definition
Each SPX subsystem must have defined mechanical, thermal, electrical, control, sensor, and serviceability interfaces before complete module integration can be treated as credible.
Independent Review and Academic Partnership
Hilgart Aerospace is pursuing university and technical review partners to challenge assumptions, evaluate materials, support trade studies, and generate independent engineering data.
Milestone-Based Subsystem Investment
Capital deployment is being organized around specific subsystem deliverables: design review, modeling, trade studies, risk reduction, prototype planning, and validation readiness.
Complete Kratos SPX Integration
The full propulsion architecture remains the long-term platform objective, but complete integration follows validated subsystem progress rather than preceding it.