HARDWARE / PRODUCTAdded 11 Jul 2026

Arcos

Pangea Aerospace
Arcos

Pangea's flagship methalox aerospike engine platform (second stage: 750 kN) -- the world's first tested LOX/methane aerospike, offering altitude-compensating efficiency for launcher first stages, second stages, boosters and reusable re-entry.

Typed specifications3 values

Discloses 2 of 10 fields engineers filter by in this category (category median 3).

Thrust
750 000 000 mN
product page
Propellant
oxygen
product page methane

Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.

As published by the supplier8 lines, in the manufacturer's own wording
Propellants
LOX / Methane (methalox)
Thrust (second stage)
750 kN
Cycle
Gas generator (open cycle)
Nozzle
Aerospike -- altitude-compensating, efficient from sea level to vacuum
Combustion chamber
Modular, deep-throttleable, bi-material additively manufactured
Interface
Adjustable interface ring for multi-stage/vehicle integration
Applications
First stage, second stage, boosters, launcher re-entry/reuse
Recognition
Winner, European Commission Prize for Game-Changing Innovation for European Launchers (Jan 2026, EUR 950,000)

About

ARCOS is Pangea Aerospace’s flagship aerospike propulsion platform and the company’s core technological breakthrough: the world’s first methane/liquid-oxygen (methalox) aerospike engine successfully built and hot-fire tested. Unlike conventional bell-shaped nozzles, an aerospike nozzle maintains near-optimal expansion efficiency at any altitude or ambient pressure, a concept long pursued in the industry but historically blocked by extreme thermal, structural and manufacturing complexity. Pangea’s success igniting a methalox aerospike proved the concept viable in practice, and ARCOS translates that milestone into a modular, scalable engine architecture whose thrust level, geometry and interface configuration can be adapted to a wide variety of launcher sizes — the second-stage configuration delivers 750 kN of thrust. Key subsystems include an adjustable interface ring for easy integration across stages and vehicle configurations, a modular, deep-throttleable, high-pressure combustion chamber that is bi-material additively manufactured for optimal thermal and structural performance, the aerospike nozzle geometry itself for altitude-adaptive efficiency, and a simple, reliable, well-proven gas-generator open engine cycle. ARCOS is designed for first-stage, second-stage, booster and launcher re-entry/reuse applications, and is already referenced by several launcher programs (Atlas, ITAN, ESPER, ARES, MERLIN and private clients). In January 2026 ARCOS won the European Commission’s Prize for Game-Changing Innovation for European Launchers (EUR 950,000), and Pangea has separately been selected by the European Space Agency to progress ARCOS subsystem validation and a flight-oriented engine architecture through 2026 as part of Europe’s push for reusable-launcher technological sovereignty.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: www.pangeapropulsion.com ↗

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