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NASA's Space Launch System Progress Report
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Space Launch System: SLS B1 and B1B Cargo Performance for Europa Clipper
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NASA's Space Launch System: Launch Capability for Lunar Exploration and Transformative Science
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Comparison of Space Launch System Aerodynamic Surface Pressure Measurements from Experimental Testing and CFD
A comparison of surface pressure coefficient measurements obtained using pressure-sensitive paint (PSP) measurements with predictions from the computational fluid dynamics (CFD) code FUN3D is presented for the NASA SLS Block 1B crew vehicle. Overall, the flow features over the SLS configuration were captured by both the PSP data and CFD data at freestream Mach numbers (M(sub ∞)) of 0.8 and 1.3. Overall, the flow features over the SLS are captured by the PSP data but the intensities of large pressure gradients are less intense than what was predicted by the CFD data. Several examples of this observation are given including the flow interaction at the booster nose cone edge, core body, and forward booster attachment hardware at M(sub ∞) = 0.8.
Testing and Analysis Correlation of Composite Sandwich Longitudinal Bonded Joints for Space Launch Vehicle Structures
The NASA Composite Technology for Exploration (CTE) Project has been developing and demonstrating critical composite technologies with a focus on joints; incorporating materials, design/analysis, manufacturing, and tests that utilize NASA expertise and capabilities. The CTE project has focused on the development of composite longitudinal bonded joint technologies for conical structures such as the SLS Payload Attach Fitting (PAF) due to challenging joint geometries and loads compared to cylindrical jointed structures. The CTE team selected and designed a double-lap composite bonded joint as the most advantageous longitudinal joint to advance for the CTE project. This paper reports on the longitudinal bonded joint sub-element test articles that were fabricated and tested for several loading conditions to test the capability of the bonded joint design. Test and analysis correlation to the sub-element test articles are presented in the paper.
Fabrication of NASA’s New Space Launch System (SLS) Driven by New Technology
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Space Launch System Launch Windows and Day of Launch Processes
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Space Launch System Engine Out Capability
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Post-Flight Reconstruction Approach for Space Launch System Artemis 1Mission
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NASA's Space Launch System Progress Toward The Launch Pad
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Space Launch System Flight Readiness Analysis Cycle Approach
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NASA's Space launch System begins integration, stacking in preparation for Artemis I
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Guidance Modifications and Enhancements for Space Launch System Block-1 in Support of Artemis I and Beyond
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NASA's Space Launch System Begins Moving to the Launch Site
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