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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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MEDPRAT Segments: Medical Risk and Capabilities on Multi-Crew, Multi-Vehicle Missions
The Medical Extensible Dynamic Probabilistic Risk Assessment Tool (MEDPRAT) is a computational model used to help quantify the medical component of spaceflight medical risk.
Shapeshifter: A Multi-Agent, Multi-Modal Robotic Platform for Exploration of Titan
UNKNOWN
Multi-mission multi-instrument data analysis software for exoplanet exploration
No abstract provided
Strengths and Weakness of Using Multi-Instrument, Multi-Mission Climate Data Records To Understand How the Earth System Is Changing
No abstract provided
The Advanced Multi-Mission Operations System (AMMOS): An Introduction to the Multi-Mission Tools and Services Used by 70+ NASA Missions
No abstract provided
Multi-wavelength, Multi-technique Searches for Planets in the Alpha Cen AB System
No abstract provided
Linear Covariance Techniques to Analyze a Multi-Vehicle, Multi-GN&C System with Applications to Rendezvous in a Near Rectilinear Halo Orbit
Typically for a rendezvous and docking scenario, only a single vehicle is considered the active vehicle. As a result, the target vehicle’s GN&C system is typically not a factor in the integrated performance analysis as it assumes a passive role. However, for upcoming NASA Artemis missions the active vehicle is both the chaser and target spacecraft. In addition, both vehicles are cooperating with one another, sharing telemetry data, and relying on data extracted from the GN&C system of the other. The process also includes a team of ground support personnel in mission control are tracking and monitoring each spacecraft uplinking state estimates and targeting solutions to support mission operations and enhance the onboard flight system performance. Being able to quickly analyze the impact of both vehicles with two different GN&C systems that also interact with the ground that does its own navigation and targeting uploads is critical. This paper outlines how to perform this rapid analysis using linear covariance techniques and applies them to a rendezvous scenario initiated in low lunar orbit and completed in a Near Rectilinear Halo Orbit (NRHO) representative of the NASA Artemis III mission.
Towards Improved Time-Series InSAR Analysis With A Multi-Depth Multi-Focusing Time-Domain Backprojection SAR Algorithm
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Atomistic Multi-Lattice Kinetic Monte Carlo (Kmc) Modeling of Hyperthermal Oxidation of Multi-Layer Graphene
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The Use of Multi-Mission Datasets in NASA DEVELOP Projects: How the Harmonized Landsat and Sentinel-2 Product and Multi-Source Land Imaging Land Surface Phenology Product Provide Solutions to Temporal Resolution Constraints for Vegetation Monitoring
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Multi-Moded Multi-Frequency Fast Single Bunch Beam Diagnostic Instrument
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Exploring Uncertainties in Multi-Input-Multi-Output (MIMO) Testing.
Abstract not provided.