HTP / Fuel Spacecraft Propellant Loading System
May 2026 - August 2026
Fluid Commodities: High-Test Peroxide / Fuel / High Pressure GN2
Pump-fed fill architecture
Meant to support simultaneous W-series spacecraft test and launch campaigns
Owned build, integration, and activation testing of propellant loading systems, including the following:Â
Component sourcing and panel fabrication
Component-level testing
System activation and checkouts (click checks, individual component functionality checks and troubleshooting, leak checks, proofing)
Test procedure authoring
Full system qualification testing to verify system functionality and fill accuracy
Manufacturing and testing resulted in doubling Varda's propellant fill capabilities for spacecraft test and launch operations
Requirements capture and mechanical and fluid system design of an upgraded automated version
Ensured adherence to 91-710 range requirements, SpaceX Falcon 9 RPUG, and ASME Boiler and Pressure Vessel Code
Updated fluid system schematic/P&ID to decrease total time for spacecraft fill operations by 50%