Engineering Capabilities

Full-stack propulsion engineering.

From the combustion chamber out to the test stand, every discipline of a liquid-rocket engine is owned, modelled, and validated in-house.

C-01

Combustion & Injectors

Injector atomisation, propellant mixing, and combustion stability — designed for clean, efficient burns across the operating envelope.

C-02

Regenerative Cooling

Cooling-channel geometry and coupled thermal-fluid analysis that keep wall temperatures within margin under peak heat flux.

C-03

Feed & Pressurisation

Blowdown and pressure-fed architectures — tankage, valves, and feed lines characterised across the full depletion cycle.

C-04

Structures & FEA

Thermal-mechanical and modal analysis verifying structural margin under launch loads, vibration, and combustion environments.

C-05

CFD & Thermodynamics

Reacting-flow CFD and cycle modelling — performance prediction, parametric sweeps, and sensitivity studies that close the loop.

C-06

Test & Instrumentation

Hot-fire test campaigns with high-rate data acquisition — pressure, thrust, and thermal telemetry feeding back into design.

R&D Infrastructure

A disciplined engineering pipeline.

Every design decision flows through a tightly integrated toolchain — from geometry definition to validated, documented results.

  1. CAD

    SolidWorks & Siemens NX

    Parametric CAD architecture for chambers, injectors, and feed assemblies — combining SolidWorks agility with Siemens NX for high-fidelity assembly modelling and manufacturing-grade definition.

  2. CFD · FEA

    Ansys

    Fluid dynamics for combustion and cooling flows, paired with structural analysis for thermal-mechanical margin verification under peak operating loads.

  3. Compute

    MATLAB

    Thermodynamic post-processing and automation — performance-curve generation, parametric sweeps, and sensitivity studies that close the simulation loop.