Rocket Propulsion Technology
Abstract
This project develops and demonstrates rocket propulsion technologies for space access and space maneuver. Analytical and experimental areas of emphasis are propellants, propellant management, combustion, rocket material applications, and innovative space access and in space propulsion concepts. Technologies of interest will improve reliability, performance, survivability, affordability, and environmental compatibility of these systems. Develop technologies to reduce the weight and cost of components using new materials and improved designs and manufacturing techniques. All efforts in this project contribute to the sustainment and growth of the space and rocket propulsion industry, providing space access and in space propulsion technology for the entire Department of Defense (DoD). Technologies under this project enable capabilities of interest to DoD, National Aeronautics and Space Administration (NASA) and growing Space community. Tasks include: proof of concept tests of critical components; advanced component development; and ground-based tests. This project develops next generation of physics-based modeling, simulation, and analysis (MS&A) tools for rapid and agile space access and in-space propulsion design, analysis, and production, as well as the digital engineering concepts to manage the entire process of design, test, and validation of space access and in-space systems. All thrusts are reviewed by a DoD level steering committee yearly for relevance to DoD missions, and the associated support costs.
Document Details
- Document Type
- Project
- Publication Date
- Oct 01, 2025
- Source ID
- 624847_1206601SF_2_3620F_PB_2025
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