Chemical Propulsion
Development and analysis of combustion, feed, cooling, nozzle, and propellant systems for high-thrust mission phases.
DEVOWER / Program 01
DEVOWER is developing and evaluating chemical and electric propulsion architectures for launch, maneuvering, transportation, and long-duration operation beyond Earth.
Development and analysis of combustion, feed, cooling, nozzle, and propellant systems for high-thrust mission phases.
Investigation of high-efficiency thrusters, power processing, propellant systems, and spacecraft integration for long-duration operation.
Engineering Scope
The program considers the components, interfaces, power, storage, and thermal behavior required to operate as one system.
Chamber and injector architectures evaluated through requirements, analytical work, modeling, and future testing.
Flow expansion, turbomachinery, valves, delivery systems, and pressure-management concepts developed as an integrated path.
Thermal-management concepts intended to protect propulsion hardware and support repeatable operation.
Propellant compatibility, cryogenic storage, conditioning, and spacecraft-level interfaces considered from the beginning.
High-efficiency propulsion concepts developed alongside the electrical systems required to operate them.
Propulsion performance evaluated against power availability, heat rejection, mass, mission duration, and vehicle architecture.
Program Boundary
DEVOWER discusses the purpose and engineering categories of its propulsion work publicly. Exact geometry, proprietary calculations, manufacturing drawings, and internal performance data are not published here.
Connected Architecture
See how propulsion, spacecraft, planetary infrastructure, resources, and energy develop into one mission architecture.
View System Roadmap