Space Launch System Scale Model Acoustic Test Ignition Overpressure Testing
No abstract available
Nance, Don↗
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Results for “space launch”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Update on Risk Reduction Activities for a Liquid Advanced Booster for NASA's Space Launch System
No abstract available
Crocker, Andy↗
Recent Flight Control System Analyses in Support of Space Launch System
No abstract available
Wall, John↗
NASA'S Space Launch System Mission Capabilities for Exploration
No abstract available
Creech, Stephen D.↗
Space Launch System Scale Model Acoustic Test Liftoff Results and Comparisons
No abstract available
Houston, Janice↗
Space Launch System Base Heating Test: Environments and Base Flow Physics
NASA MSFC and CUBRC designed and developed a 2% scale SLS propulsive wind tunnel test program to investigate base flow effects during flight from lift-off to MECO. This type of test program has not been conducted in 40+ years during the NASA Shuttle Program. Dufrene et al paper described the operation, instrumentation type and layout, facility and propulsion performance, test matrix and conditions and some raw results. This paper will focus on the SLS base flow physics and the generation and results of the design environments being used to design the thermal protection system.
Mehta, Manish↗
Space Launch System Base Heating Test: Tunable Diode Laser Absorption Spectroscopy
No abstract available
Parker, Ron↗
Space Launch System Base Heating Test: Experimental Operations and Results
No abstract available
Dufrene, Aaron↗
Overview of the Space Launch System Ascent Aeroacoustic Environment Test Program
No abstract available
Herron, Andrew J.↗
Requirements and Verification (R&V) Streamlining for NASA's Space Launch Systems (SLS)
No abstract available
Whitehead, Josh↗
Modeling and Test of Space Launch System Core Stage Thrust Vector Control
No abstract available
Orr, Jeb S.↗
Overview of the Space Launch System Transonic Buffet Environment Test Program
No abstract available
Piatak, David J.↗
NASA's Space Launch System Transitions From Design To Production
No abstract available
Askins, Bruce R.↗
Update on Risk Reduction Activities for a Liquid Advanced Booster for NASA's Space Launch System
Dynetics has designed innovative structure assemblies; manufactured them using Friction Stir Welding (FSW) to leverage NASA investments in tools, facilities, and processes; conducted proof and burst testing, demonstrating viability of design/build processes Dynetics/AR has applied state-of-the-art manufacturing and processing techniques to the heritage F-1, reducing risk for engine development Dynetics/AR has also made progress on technology demonstrations for ORSC cycle engine, which offers affordability and performance for both NASA and other launch vehicles Full-scale integrated oxidizer-rich test article. Testing will evaluate performance and combustion stability characteristics. Contributes to technology maturation for ox-rich staged combustion engines.
Crocker, Andy↗