Subsystem Funding Range
Based on current planning, each major SPX subsystem may require approximately $300,000 to $1,000,000 to move from design review through engineering refinement, prototype planning, technical validation, and independent review. Actual costs may vary based on material selection, test requirements, university or laboratory engagement, fabrication complexity, and validation scope.
Thermal Management System
$300K–$1M
Thermal-power balance modeling, coolant trade study, materials review, radiator sizing, thermal spine analysis, and validation planning.
Thermal / Electric Auxiliary Power
$300K–$1M
Waste heat recovery analysis, Brayton-cycle integration studies, power routing, efficiency modeling, and subsystem interface definition.
Multi-Gas Combustion / Plasma
$300K–$1M
Gas-ring design review, mixture control, flow balance, pressure stability, material exposure, and combustion-plasma validation planning.
Magnetic Velocity & Flow Stabilization
$300K–$1M
Magnetic field architecture, propellant-flow stabilization, interface controls, thermal exposure effects, and performance modeling.
Plume / Exhaust Control System
$300K–$1M
Plume shaping, vector-control concepts, thermal and structural loading, exhaust stability, and subsystem validation requirements.
H.U.M.A.N™ AI Control System
$300K–$1M
Sensor integration, diagnostics, fault response, autonomous decision support, subsystem coordination, and control-logic validation.