High-density rocket propulsion

Rocket engines.Engineered from the fuel up.

Space Frontier combines new fuels and advanced manufacturing to unlock the potential of hybrid propulsion.

Hybrid propulsion system with its fuel grain visible inside
CAD ASSEMBLY / FUEL GRAIN VISIBLESCROLL TO EXPLORE ↓

01 / SAFETY

Non-explosive architecture

Fuel and oxidizer remain physically separated until operation, supporting safer handling and integration.

02 / SIMPLICITY

Fewer components.
Easier integration.

Compared with liquid-propellant architectures, hybrid systems can reduce plumbing and component count, with potential benefits for size, cost and integration.

03 / VERSATILITY

Fuel tailored
to the mission

High-density formulations and printed grain architectures let us design around different operating profiles, from satellite propulsion to atmospheric flight.

SCIENTIFIC
PARTNERS
INCUBATED ATESA BIC Lazio

02 / THE LABORATORY

Automated testing.
Controlled conditions.

A dedicated infrastructure for fuel characterisation, propulsion testing and digital-twin development. Mechanical, electronic and control systems are designed; construction and commissioning are the next steps.

01 AUTOMATED02 REMOTELY CONTROLLED03 TIMED TEST SEQUENCES

Inside the laboratory.

DESIGNED · TO BE BUILT
Cutaway CAD of the containerised laboratoryCAD / CONTAINERISED LABORATORY

Cutaway CAD view.

Liquid N₂O.
Non-cryogenic storage.

The oxidizer supply line is developed with SPF Impianti using certified components.

Controlled feed conditions are designed to support comparable fuel-testing campaigns without cryogenic storage infrastructure.

03 / MARKET & APPLICATIONS

One platform.
Multiple applications.

The same engineering core is configured for satellite propulsion, solid turbojets and hypersonic operating profiles.

Explore market & applications ↗

CUSTOMERS · PARTNERS · INVESTORS

Build the next propulsion
system with us.

Open a conversation ↗

COMPONENT FOCUS / OXIDIZER

Choosing the
oxidizer.

Two possible oxidizers, with different storage and handling considerations.

N₂O

Nitrous oxide

Advantages

  • Self-pressurizing behaviour can simplify the feed-system architecture.
  • Non-cryogenic storage and established use in hybrid propulsion.

Trade-offs

  • Storage pressure varies with temperature.
  • Two-phase flow can complicate delivery behaviour.
  • Decomposition hazards require dedicated safety assessment.
H₂O₂

Hydrogen peroxide

Advantages

  • Can be stored as a non-cryogenic liquid.
  • Catalytic decomposition produces water vapour and oxygen.

Trade-offs

  • Long-term stability depends on material compatibility and purity.
  • Concentrated peroxide requires controlled handling.
  • Catalyst durability must be assessed where catalytic decomposition is used.

Oxidizer selection depends on the application and validation programme.

NASA · Nitrous oxide ↗ESA · Hydrogen peroxide ↗

COMPONENT FOCUS / OUR FUELS

3D-printed fuels.
Measured from within.

Formulation, printed geometry and tomographic inspection connect the digital definition of each grain with its measured behaviour.

3D-PRINTED BIOPLASTIC GRAIN

Drag the line upwards to reveal the tomography.

MATERIAL RENDERINGIllustrative rendering
CT SURFACECT-reconstructed geometry

Same geometry, two views. Material rendering and CT-reconstructed surface.

Star grain · 3D-printed bioplastic sample.

01 / REGRESSION

Point-by-point
regression control

Material and local geometry are design variables. CT comparison reveals how the grain changes at each location, beyond an average diameter.

02 / PRODUCTION

Replicability

A digital grain definition and recorded printing parameters support repeatable manufacturing and comparison between batches.

03 / INSPECTION

Micrometric
quality control

Tomographic inspection measures internal geometry and detects voids and local defects to compare the produced grain with its design.

A traceable production and test record provides more precise, relevant data for AI training and regression-model development.