J-2X (Engine)

The J-2X is a modern expander cycle, bi-propellant rocket engine, planned for use in the Ares I and Ares V launch vehicles. It consumes liquid hydrogen and liquid oxygen. It has its origin in the J-2 rocket engines used by the Saturn Ib and Saturn V launchers. It is produced by Rocketdyne.

Differences from the J-2

While the J-2 was a gas-generator cycle or open cycle rocket engine, the J-2X uses an expander cycle (also called closed cycle) for powering its turbopumps. In this engine cycle, the propellant, which gets used for regenerative cooling of chamber and nozzle is also used to drive a turbine, which provides power to the turbopumps.

This article is a stub. You can help Orbiterwiki by expanding it.