Desert Work Propulsion provides gridded‑ion electric propulsion systems for long‑duration space missions, handling the full development cycle from requirement definition through component testing and qualification planning.
Funding
Funding not disclosed
Founders
Product
Problem
Space missions that require high delta‑V, long total impulse, and extended operational life often lack propulsion options that combine high thrust density with efficient power use, leading to oversized fuel tanks and limited mission flexibility. Existing ion and Hall‑effect thrusters may not meet the performance or scalability needed for modern government, defense, and commercial spacecraft.
Solution
Desert Work Propulsion (DWP) delivers gridded‑ion electric propulsion systems that address these constraints through a full‑service development model, from requirement definition and architecture trade studies to component testing, life‑modeling, and qualification planning. Their patented Annular Ion Engine (AIE) provides superior thrust density and thrust‑to‑power ratios compared with traditional ion and Hall‑effect thrusters, enabling higher performance in a compact form factor. The modular IONPRO™ series offers reconfigurable thruster configurations that can be tailored to specific mission profiles while reducing development cost and schedule risk. DWP’s in‑house, state‑of‑the‑art testing facility supports cost‑effective validation of high‑voltage hardware, plasma diagnostics, and thrust‑stand measurements. By offering expertise as a service, DWP eliminates the need for customers to build internal electric‑propulsion teams, accelerating technology adoption and reducing program uncertainty.
Target Audience
Primary customers are government and mission owners (including defense and national‑security agencies) as well as commercial space companies that require high‑performance electric propulsion for long‑duration, high‑delta‑V missions.
Features
- Annular Ion Engine architecture delivering higher thrust density and thrust‑to‑power ratio than conventional ion or Hall‑effect thrusters
- Patent‑pending IONPRO™ modular thruster series that can be reconfigured for a wide range of power levels and mission requirements
- Full‑cycle program support: requirement definition, architecture trades, life‑modeling, qualification planning, and hardware execution
- In‑house, high‑voltage test facility with plasma diagnostics, thrust stands, and data‑acquisition systems for rapid, cost‑effective validation
- Design and fabrication of thruster components, power processor units, and high‑voltage test support equipment
- Development of custom power electronics, plasma diagnostics, and integration tools for spacecraft‑thruster interfaces
- Consultation services covering manufacturing challenges, test protocol formulation, flight sequence development, and mission operations support