Abstract: The NDARC code performs design and analysis tasks. The design task involves sizing the rotorcraft…
Author: New NASA STI
Recent Advancements in the Infrared Flow Visualization System for the NASA Ames Unitary Plan Wind Tunnels
Abstract: The following details recent efforts undertaken at the NASA Ames Unitary Plan wind tunnels to…
Optimal Growth in Hypersonic Boundary Layers
Abstract: The linear form of the parabolized linear stability equations is used in a variational approach…
Hot-Fire Test Results of an Oxygen/RP-2 Multi-Element Oxidizer-Rich Staged-Combustion Integrated Test Article
Abstract: As part of the Combustion Stability Tool Development project funded by the Air Force Space…
Enabling Autonomous Propellant Loading: Providing Situational Awareness Through Model Based Reasoning
Abstract: No abstract available
Combustion Dynamics and Stability Modeling of a Liquid Oxygen/RP-2 Oxygen-Rich Staged Combustion Preburner and Thrust Chamber Assembly with Gas-Centered Swirl Coaxial Injector Elements
Abstract: The Combustion Stability Tool Development (CSTD) project, funded by the Air Force Space and Missile…
Additively Manufactured Low Cost Upper Stage Combustion Chamber
Abstract: Over the past two years NASA's Low Cost Upper Stage Propulsion (LCUSP) project has developed…
Design and Fabrication of Oxygen/RP-2 Multi-Element Oxidizer-Rich Staged Combustion Thrust Chamber Injectors
Abstract: As part of the Combustion Stability Tool Development project funded by the Air Force Space…
A Framework for Assessing the Reusability of Hardware (Reusable Rocket Engines)
Abstract: Within the space flight community, reusability has taken center stage as the new buzzword. In…
Overview of Marshall Space Flight Center Activities for the Combustion Stability Tool Development Program
Abstract: This presentation covers the overall scope, schedule, and activities associated with the NASA - Marshall…