PROPULSION ARCHITECTURE · GEN-4

Magnetohydrodynamic Drive Systems

Zero-moving-part electromagnetic propulsion leveraging Lorentz force acceleration across conductive media. Engineered for aerospace, subsurface, and high-altitude platforms requiring silent, high-thrust, and maintenance-minimized operation.

Operating Principle

MHD drives generate thrust by interacting orthogonal magnetic and electric fields with ionized or electrically conductive fluid. Unlike conventional mechanical propulsion, Aevum Zenth's architecture eliminates rotating assemblies, reducing vibration signature, maintenance cycles, and acoustic emissions by up to 94%.

Power Bus

DC 1.2–4.8 kV

Field Coils

Superconducting

Plasma / Fluid Channel

Ionized medium

Thrust Vector

Electromagnetic

Control Matrix

Real-time B/I modulation

Exhaust / Flow

Low acoustic signature

Performance Specifications

Validated across multiple test envelopes. Data reflects nominal operating conditions at sea level / 1 atm unless noted.

ParameterValue
Max Thrust (Continuous)42.5 kN
Peak Thrust (Pulse)68.0 kN (≤4.2s)
Specific Impulse (Isp)1,850–3,200 s
Power Density8.4 kW/kg (system)
Mass Flow RateAdaptive (0.12–0.85 kg/s)
Operational EnvelopeVacuum to 12 km altitude / Subsurface
Acoustic Signature< 28 dB(A) @ 1m
Control Latency≤ 4 ms (closed-loop)

Application Domains

MHD drive configurations are adapted for platform-specific fluid dynamics, thermal management, and mission profiles.

Orbital & Interplanetary

Electric propulsion for station-keeping, trajectory correction, and high-Isp deep-space transit. Compatible with xenon, krypton, and inert gas propellants.

AEROSPACE DIV.

Subsurface Vessels

Silent electric drive for naval research, deep-sea exploration, and autonomous underwater platforms. Saltwater acts as native conductive medium.

MARINE / DEFENSE

High-Altitude UAVs

Boundary-layer ionization for stratospheric endurance flight. Reduces mechanical complexity and enables distributed propulsion architectures.

ADVANCED AVIATION

Industrial & Scientific

Plasma confinement, material processing, and experimental fluid dynamics testing. Custom channel geometries available via Zenth Advanced Research.

R&D INTEGRATION

Development Pipeline

Current engineering milestones and qualification roadmap for Gen-4 MHD architectures.

Conceptual Design
Component Validation
Subsystem Integration
4
Flight/Sea Qualification
5
Mass Production

* Current phase: Environmental stress screening & mission-profile endurance testing. Expected TRL-8 transition: Q3 2027.

Engineering Integration

Access technical datasheets, control API documentation, platform integration matrices, and request a custom propulsion architecture consultation.