SBIR-STTR Award

Launcher E-2: Highest-Performance 3D Printed Liquid Rocket Engine to Reduce Cost of Dedicated Small Satellite Launch
Award last edited on: 6/15/2023

Sponsored Program
SBIR
Awarding Agency
DOD : AF
Total Award Amount
$2,498,261
Award Phase
2
Solicitation Topic Code
AF192-001
Principal Investigator
Maxime Haot

Company Information

Launcher Inc

12624 Daphne Avenue
Hawthorne, CA 90250
   (212) 380-7533
   hi@launcherspace.com
   www.launcherspace.com
Location: Single
Congr. District: 07
County: Kings

Phase I

Contract Number: FA8649-19-P-A085
Start Date: 8/2/2019    Completed: 8/2/2020
Phase I year
2019
Phase I Amount
$49,920
The Department of Defense (DoD) and Department of the Air Force (AF) have identified access to responsive, low-cost, small satellite launch systems as a key capability and priority for their space mission sets. Launcher's E-2 liquid rocket engine (thrust: 22,000 lbf) is low cost (3D printing) and will be the highest performance rocket engine for small launch vehicles with 327s specific impulse (ISP) for the booster version and 365s ISP for the second stage version. Launcher's E-2 engine will advance affordable small satellite launch vehicle technologies as its higher performance design materially increases a rocket's payload capacity by consuming less propellant while generating the same thrust. As a result, Launcher's E-2 liquid rocket engine also reduces the price to deliver small satellites to orbit which is a key capability and priority for the Air Force.

Phase II

Contract Number: FA8808-20-C-0007
Start Date: 11/5/2019    Completed: 11/5/2021
Phase II year
2020
(last award dollars: 2022)
Phase II Amount
$2,448,341

The Department of Defense (DoD) and Department of the Air Force (AF) have identified access to responsive, low-cost, small satellite launch systems as a key capability and priority for their space mission sets. Launcher's E-2 liquid rocket engine (thrust: 22,000 lbf) is low cost (3D printing) and will be the highest performance rocket engine for small launch vehicles with 327s specific impulse (ISP) for the booster version and 365s ISP for the second stage version. Launcher's E-2 engine will advance affordable dedicated small satellite launch vehicle technologies as its higher performance design materially increases a rocket's payload capacity by consuming less propellant while generating the same thrust. As a result, Launcher's E-2 liquid rocket engine also reduces the price to deliver small satellites to orbit which is a key capability and priority for the Air Force. This Phase II Work plan will advance the development of Launcher's E-2 liquid rocket engine. Specifically, we will test-fire the Launcher E-2 injector and combustion chamber for the first time and prove the design is operational while demonstrating the specific impulse performance claim above.