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MILESTONE: Launcher’s 3D-Printed E-2 Rocket Engine Achieves Full Thrust at NASA Stennis Space Center

NASA Stennis Space Center
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April 25, 2022

On Thursday April 21, 2022, Launcher’s E-2 liquid rocket engine successfully demonstrated nominal thrust, pressure and oxidizer/fuel mixture ratio for the first time in a test fire at NASA Stennis Space Center.

E-2 is a closed cycle 3D-printed, high-performance liquid rocket engine in development for the Launcher Light launch vehicle (inaugural launch scheduled for 2024). A single E-2 engine will boost Launcher Light to low Earth orbit with 150 kg of payload.

Data from Thursday’s successful test fire of the E-2 engine:

  • 10 metric tons of thrust (22,046 lbf).
  • 100 bar (1,450 psi) of combustion pressure.
  • Highest performance 2.62 propellant mixture ratio for LOX/Kerosene at 100 bar of pressure.
Launcher E-2 thrust chamber assembly on its test stand at NASA Stennis Space Center. (Credit: Launcher/John Kraus Photography)

E-2’s chamber is uniquely liquid oxygen cooled and 3D-printed in copper alloy in a single piece. It also uses industrial supply chain copper chromium zirconium alloy (CuCrZr), reducing costs and supply chain constraints compared to aerospace-grade copper alloy typically used in 3D-printed combustion chambers.

Launcher is the first small launch company to use 3D-printed copper alloy, and leads in small launch 3D-printed technology with its development of the first large format (100 x 45 x 45 cm) custom 3D printer in partnership with AMCM. Launcher's single-part copper alloy combustion chamber is produced on an AMCM M4K 3D printer.

In addition, E-2's state of the art co-axial injector is 3D-printed on a Velo3D Sapphire.

These technologies enable higher performance which translates into more payload per rocket and lower prices for Launcher customers.

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Demonstrating its reusability, the chamber was in perfect condition after 40 seconds of total test fire time. Photo of actual chamber throat after tests below.

Launcher E-2 Combustion Chamber Throat was in perfect condition after the test campaign.

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As a next step, Launcher tests again in early May with the same chamber and injector, lightly reworked to remove all film cooling—which increases performance. The goal is to increase C* efficiency from 90% in this test to our 98% target⁠—and perhaps see  our trademark blue Mach diamonds for this liquid oxygen/kerosene based engine, a global first.

E-2 is a closed cycle engine and its high-pressure (310 bar), high-efficiency, single-shaft turbopump development is moving forward in parallel (test video). In March 2022, Launcher successfully tested E-2's turbine and liquid oxygen pump in boost mode at 130% nominal flow. Launcher expects to demonstrate a full duration, three-minute test with the E-2 integrated turbopump in closed cycle configuration in Q4 of 2022.

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