High-thrust chemical, electric, and hybrid propulsion architectures engineered for orbital insertion, deep-space transit, and precision maneuvering.
AeroVance Propulsion designs, manufactures, and test-validates propulsion systems across multiple propellant classes and mission profiles. Our engineering teams leverage advanced CFD modeling, combustion stability analysis, and materials science to deliver engines that meet stringent reliability and performance requirements.
Every system undergoes rigorous hot-fire testing, vibration qualification, and thermal vacuum simulation at our dedicated Nevada and Florida facilities before flight certification.
Scalable engine families optimized for specific impulse, thrust-to-weight ratio, and mission duration.
Liquid bipropellant and hybrid rockets for launch vehicles, upper stages, and orbital transfer vehicles. Features regeneratively cooled combustion chambers and gimbal-capable thrust vector control.
Hall-effect thrusters, gridded ion engines, and pulsed plasma thrusters for station-keeping, constellation deployment, and deep-space cargo transfer. Ultra-low propellant consumption with high delta-v capability.
Combines liquid oxidizer with solid fuel grain for inherent safety, throttleability, and rapid mission reconfiguration. Ideal for crewed vehicles, lunar landers, and small-sat launchers.
Cold gas, monopropellant, and bipropellant thruster clusters for attitude control, docking maneuvers, and deorbit operations. High cycle reliability with redundant valve architectures.
Every propulsion unit undergoes comprehensive environmental and performance validation before flight release.
| Test Protocol | Parameters Verified | Facility |
|---|---|---|
| Hot-Fire Qualification | Chamber pressure, thrust oscillation, nozzle erosion, startup/shutdown transients | Nevada Test Range (Site 4) |
| Vacuum Thermal Cycling | Cryogenic propellant compatibility, thermal expansion stress, valve actuation at -180ยฐC to +120ยฐC | Florida TVAC Chamber |
| Vibration & Acoustics | Launch environment survivability, structural resonance, fastener integrity, avionics shielding | Multi-Axis Shaker Array |
| EMI/EMC Compliance | Thruster plume interference, ignition spark isolation, telemetry signal integrity | Annechoic Test Suite |
| Long-Duration Endurance | Propellant feed stability, turbopump wear, thermal management over 10,000+ second burns | Orbital Simulation Rig |
Systems currently in flight or qualified for upcoming operational programs.
Restartable, gimbal-controlled engine delivering 145 kN thrust. Used on 38 LEO-to-GTO transfer missions with 100% success rate.
12-unit thruster cluster providing 1.2 kW total power. Enables constellation momentum management and orbital maintenance for 500+ smallsats.
Throttleable hybrid engine designed for soft-landing precision on lunar terrain. Qualified for regolith environment and cryogenic propellant handling.
Quality Management
Special Processes
U.S. Defense Export
Type Certification
ESA Space Standards
Environmental Mgmt
From custom thruster design to full engine integration and flight certification, our propulsion division provides end-to-end engineering support. Request a technical consultation or download our system specifications.