cometadata/datacite-titles-descriptions-related-identifiers huggingface dataset:
DOI: 10.48577/jpl.zpungq
title: Endurance Mission-level Simulation Architecture for Autonomy Development

description: The Endurance mission concept is a lunar sample-return mission that comprises a long-range traverse from the middle of the South-pole Aitken basin to the South Pole to collect samples from sites of high science value along the route. The samples would be returned to Earth by Artemis astronauts. This paper presents the design and development of a mission-level simulation for the Endurance mission concept, which allows us to mature the concept of operations (ConOps) and understand the need and range of onboard autonomous functions and ground operations tools. Simulation results help us understand the global traverse duration and improve inefficiencies in the current ConOps using some degree of onboard autonomy.
DOI: 10.48577/jpl.nptetl
title: A DELICATE BALANCE OF TORQUE AND THRUST: HOW LUNAR FLASHLIGHT USED ROTATING MANEUVERS TO MAKE ONE THRUSTER DO THE WORK OF FOUR

description: After launch, Lunar Flashlight (LFL) was beset by thruster failures, ultimately leaving it with only one partially-operable thruster. By developing the rotating Trajectory Correction Maneuver (TCM), the team made use of the reaction wheels to recover trajectory control capability. In this maneuver, the inertial momentum vector is rotated in a plane, while the spacecraft body momentum remains nearly stationary, by carefully balancing the thruster torque, spacecraft rotation rate, and initial momentum state.
DOI: 10.5281/zenodo.13208442
title: Frankfurt /Main Stern-Apotheke
DOI: 10.48577/jpl.h1ada1
title: Sensitivity Analysis and Validation of a Computational Framework for Supersonic Parachute Inflation Dynamics

description: The supersonic parachute inflation dynamics (PID) of the Advanced Supersonic Parachute Research (ASPIRE) SR03 parachute system, represented by a detailed computational model, are numerically simulated using a high-fidelity framework for fluid-structure interaction (FSI). Numerical results, in the form of representative quantities of interest, are validated against data from the ASPIRE SR03 flight test. The validation is performed on a predefined array of simulations in order to investigate the robustness of these results and establish their sensitivities to identified critical modeling assumptions, including: resolution of the computational fluid dynamics mesh; choice of the constitutive law for material modeling; and priority of the physics to be captured. These sensitivities are evaluated with attention to their development and computational costs, and to their associated uncertainties. The ultimate goal of the reported work is to pave the way for establishing best practices for the numerical simulation of supersonic PID; and to advance the potential role of computational FSI in the design and evaluation processes of inflatable systems in general.
DOI: 10.48577/jpl.eykwym
title: EXEP: Development of a Multiplex Application Specific Integrated Circuit driver for Deformable Mirrors

description: Deformable mirrors (DMs) are at the heart of any adaptive optics system. State-of-the-art, high-actuator count DMs suffer from external heavy and bulky electronics in which electrical connections are made through thousands of wires. To overcome this challenge, we are developing Application Specific Integrated Circuits (ASIC) capable of driving a DM in a single small package in space conditions. This integrated ASIC-DM is ideal for space missions, where it offers significant reduction in mass, power and complexity while maintaining performance compatible with high-contrast imaging of exoplanets. We successfully prototyped, package and tested a 16x16 DM-ASIC array following the Roman Space Telescope mission requirements. The ASIC chip was irradiated to a total ionizing dose equivalent to a 6-year mission in L2 orbit and tested at the Roman coronagraph specific temperature range.
DOI: 10.48577/jpl.mtonr2
title: ENHANCEMENTS TO THE ASTRODYNAMICS SOFTWARE AND SCIENCE ENABLING TOOLKIT (ASSET)

description: The Astrodynamics Software and Science Enabling Toolkit (ASSET) is a free and opensource software library enabling rapid spacecraft mission design and analysis. The software is a parallel, object-oriented C++ library, with a Python front-end for quick development, and ease-of-use. ASSET is being developed at the University of Alabama’s Astrodynamics and Space Research Laboratory (ASRL) and is funded by NASA. This paper outlines new enhancements added to ASSET since its initial release, including improved adaptive mesh refinement techniques for collocation based optimal control problems, and vectorized integration routines.
DOI: 10.48577/jpl.8zodiz
title: Preliminary Design of the Supersonic Disk-Gap-band Parachute for Sample Retrieval Lander

description: The Sample Retrieval Lander Project is a key element of the planned joint Mars Sample Return Campaign by NASA and the European Space Agency. Sample Retrieval Lander requires landing a heavier payload than has ever been attempted on Mars. In support of this endeavor, a 24-meter diameter Disk-Gap-Band parachute is under development. The increased performance requirements of this parachute have driven an extensive preliminary design phase including broadcloth development, soft confluence testing, and mortar deployment system design and test. Working with multiple industry partners, the Jet Propulsion Laboratory has completed early testing on the parachute and mortar designs for Sample Retrieval Lander, and the system is prepared for a larger verification and validation test campaign.
DOI: 10.48577/jpl.x2dcsr
title: PBL Profiling Capabilities from the HiPPO Instrument Concept

description: A new instrument concept for profiling temperature and water vapor at high vertical resolution in the troposphere and planetary boundary layer (PBL) has been studied. This concept, dubbed HiPPO, is based on crosslink radio occultation (RO) between two low Earth orbiters operating in multiple frequencies between 8-35 GHz. It preserves the many advantages of GNSS-RO while providing a more accurate temperature and water vapor retrievals. To assess the accuracy of this technique and derive instrument requirements, high-fidelity end-to-end simulations are performed under a wide range of PBL conditions and measurement noise. We present the latest simulation results, along with estimates of transmit power and antenna gains needed to achieve the desired accuracy and resolution of temperature and water vapor in the PBL.
DOI: 10.48577/jpl.nljeaz
title: On the Magnetic Fields of Ice Giants

description: No abstract available.
DOI: 10.48577/jpl.2gs4vm
title: ORBITING BELOW THE BRILLOUIN SPHERE USING TRANSLATED SPHERICAL HARMONICS

description: No abstract available.
DOI: 10.48577/jpl.jl5s5y
title: OWLAT: The Evolution of an Advanced Lander-Manipulator Testbed for Enabling Autonomy Development for Ocean Worlds Missions

description: NASA has developed platforms for evaluating autonomy technologies for lander-based robotic sampling missions to Ocean Worlds. Mission concepts that propose operations at a further distance from Earth and under constrained resources will rely more heavily on robust autonomy capabilities for mission operations. The Ocean World Lander Autonomy Testbed (OWLAT) was built in an effort to bridge the gap between autonomous technologies emerging from academia and industry, and the specific demands of lander-style mission operations. OWLAT provides a facility for testing technologies against the authentic challenges of autonomous operations in low-gravity environments. Purposefully designed to limit the implementation overhead, the testbed provides telemetry logging from the system and an adaptable interface for commanding by leveraging an open-source middle-ware suite. This paper presents the capabilities of the OWLAT testbed, a review of deployments of autonomous technologies on the testbed, and lessons learned from developing a high-fidelity, versatile testbed that facilitates the advancement of technology readiness level (TRL) for preconfigured autonomous operation solutions.
DOI: 10.48577/jpl.ncu8vi
title: 4th Body-Induced Secondary Resonance Overlap Inside Unstable Resonant Orbit Families: a Jupiter-Ganymede 4:3 + Europa Case Study

description: No abstract available.
DOI: 10.48577/jpl.m9jsqo
title: OCO-2/3 Calibration Report

description: No abstract available.
DOI: 10.48577/jpl.5qbnh1
title: Coronagraph Testbed Results

description: No abstract available.
DOI: 10.48577/jpl.yb8xtk
title: Minimum Requirements for Space System Cybersecurity - Ensuring Cyber Access to Space

description: Space systems are continuously under cyber attack. Minimum cybersecurity design requirements are necessary to preserve our access to space. This paper proposes a scalable, ex- tensible method for developing minimum cyber design principles and subsequent requirements for a space system based on any given mission priority. To test our methodology, we selected the fundamental mission priority of preserving access to space by preventing the permanent loss of control of a satellite. We then generate the minimum number of secure-by-design principles that can result in the permanent loss of control of a satellite and translate these into example minimum requirement ‘shall’ statements. Our proposed minimum requirements methodology and example can serve as a starting point for policymakers aiming to establish security requirements for the sector. Further, our methodology for establishing minimum requirements will be engaged for prioritizing the efforts of the emergent IEEE International Technical Standard for Space Cybersecurity (Working Group P3349).
DOI: 10.48577/jpl.qoyyl9
title: Compact Fire Infrared Radiance Spectral Tracker (c-FIRST)

description: No abstract available.
DOI: 10.48577/jpl.2cobdb
title: (ExEP): Coronagraph Design Survey for Future Exoplanet Direct Imaging Space Missions

description: NASA is embarking on an ambitious program to develop a Habitable Worlds Observatory (HWO) flagship to directly image ∼ 25 potentially Earth-like planets and spectroscopically characterize them for signs of life, as well as perform transformational astrophysics. This mission was recommended by Astro2020, which additionally recommended the Great Observatory Maturation Program (GOMAP), a new approach for flagship formulation based on increasing the scope and depth of early, pre-phase A trades and technology maturation. A critical capability of the HWO mission is starlight suppression. To inform future architecture trades, it is necessary to survey a wide range of technologies, from the relatively mature ones such as the ones described in the LUVOIR and HabEx reports, to the relatively new and emerging ones, which may lead to breakthrough performance. In this paper, we present a summary of an effort, funded by NASA’s Exoplanet Exoplaration Program (ExEP), to survey coronagraph architectures for HWO. In particular, our results consist of: (1) a database of different coronagraph designs sourced from the world-wide coronagraph community that are potentially compatible with HWO; (2) evaluation criteria, such as expected mission yields and feasibility of maturing to TRL 5 before phase A; (3) a unified modeling pipeline that processes the designs from (1) and outputs values for any machine-calculable criteria from (2); (4) assessments of maturity of designs, and other criteria that are not machine-calculable; (5) a table presenting an executive summary of designs and our results. While not charged to down-select or prioritize the different coronagraph designs, this survey is designed to be as informative as possible to facilitate future HWO trade studies.
DOI: 10.48577/jpl.sa4kup
title: MODELING SPACECRAFT EARTH RADIATION PRESSURE DATA TO IMPROVE SPACECRAFT TRAJECTORY ESTIMATION AND DESIGN

description: This paper examines a method to model both short and longwave radiation from the Earth and determine the net force vector applied to the spacecraft at any point in time. The Clouds and the Earth’s Radiant Energy System (CERES) project has created a data set gathered by 6 operational Earth orbiting satellites and other instruments globally. Hourly SW and LW data are incorporated into the simulation to more accurately determine the likely perturbations at various days through-out the year. This force can be integrated continuously to examine the effect of ERP on trajectory dispersions. Models for the Earth perturbations of interest, and spacecraft trajectory propagation under the main disturbances are simulated using JPL’s MONTE tool. Results for the expected ERP acceleration are presented for a 1000 km Earth orbit with various spacecraft shapes using some common orientations throughout the year. ERP is commonly mod-eled with as few as 6 coefficients that represent the reflected SW and emitted LW energy that is averaged over the entire year and tends to be longitude independent. By incorporating data sets that vary dynamically in both the spatial and time domains, a more accurate near real-time solu-tion for ERP can be estimated. This is expected to result in more accurate orbital propagation re-sults that would reduce the dispersions and covariance. MONTE is able to incorporate spacecraft shape models that more accurately model the accelera-tions in a particular direction. For this paper spherical, cylindrical, plate, and cubic shapes are ex-amined. The latter three shapes are attitude dependent so a few common orientations are examined to show the variance of acceleration with shape and orientation. Orientations examined include shape axis pointing for nadir, zenith, sun pointing, surface tracking and inertial hold. By varying spacecraft shape and orientation, their effect will show additional dispersions in acceleration and the resulting propagation over time.
DOI: 10.48577/jpl.cpq9du
title: I Put a Resonance Inside Your Resonance So You Can Overlap While You Overlap: Why 4th-Body Effects are Important in Multi-Moon Systems

description: No abstract available.
DOI: 10.48577/jpl.2lc2s1
title: Permeability Modeling of Mars Parachute Broadcloth Materials

description: The broadcloth material used in parachute manufacturing is generally a thin, woven, permeable textile. The relatively small length scales of the pores and gaps inside the fabric make it challenging to resolve these features in a full-scale parachute simulation. Simulations are performed using a 3D reconstruction the geometry of the material used in the Mars 2020 mission, and simulation results using the detailed reconstructed geometry are compared to the simplified model previously proposed in (Huang, D. Z.,Wong, M. L., Lele, S. K., and Farhat, C., “Homogenized Flux-Body Force Treatment of Compressible Viscous Porous Wall Boundary Conditions,” AIAA Journal, Vol. 59, No. 6, 2021, pp. 2045–2059). Furthermore, results from simulations under Earth ambient lab conditions are compared to experimental permeability test data to verify the choice of a simplified geometry required for some reduced-order models. A series of simulations under ASPIRE SR03 flight conditions are also performed to study the permeability of the fabric in a rarefied flow regime. The flow inside the material is shown to be similar to a developing pipe flow that does not reach a fully developed state. Significant slip velocity is observed inside the individual pores in the material, and the pressure drag is found to be the primary contributor to the overall material drag. The previous analytical pipe flow solution based on a simplified pore geometry solution predicts a higher total drag by only a small amount (∼ 0.8%) compared to the results presented in this work. Therefore, while flow through the parachute material at the micro-scale shows interesting physics, adding more complex assumptions to simplified models, such as a slip wall boundary condition and rarefied effects, likely increases the computational cost and complexity without significantly changing the predicted drag on the material.
DOI: 10.48577/jpl.xhykfw
title: Quasi-Periodic Near-Rectilinear Halo Orbits For Enceladus Jet Targeting

description: No abstract available.
DOI: 10.5281/zenodo.13208446
title: Frankfurt /Main Apotheke Am Eschenheimer Turm

description: Historical questionnaire/s 1924/1948 and index cards, partly selected enclosures regarding the history of a German pharmacy, catalogued via Kalliope portal (Historischer Fragebogen 1924/1948 und Karteikarten, ggf. gemeinfreie Anlagen zur Apothekengeschichte; als Katalog dient das Nachlassportal Kalliope): https://kalliope-verbund.info/DE-611-BF-70963 [Funktion: Im Findbuch anzeigen]Please note: The Kalliope catalogue entry might indicate related material in the archival folder which cannot be published due to copyright or other legal restrictions (NB: Das Katalogisat bei Kalliope kann auch auf Materialien - teils erheblichen Umfangs - verweisen, die aus archiv- oder urheberrechtlichen Gründen nicht veröffentlicht werden dürfen).
DOI: 10.48577/jpl.tur4wh
title: Exoplanet Atmospheres from a Transit Spectroscopy Perspective

description: No abstract available.
DOI: 10.48577/jpl.dnszix
title: Cosmology from the Diffuse Emission in the Extragalactic Background Light

description: No abstract available.
DOI: 10.48577/jpl.trwayo
title: Presentation: Exoplanet detection techniques for direct imaging dark zone maintenance data sets

description: No abstract available.
DOI: 10.48577/jpl.nlrjur
title: Initial Statistical Analysis of Long-Term Averaged Solar Wind as the Internal Charging Environment

description: No abstract available.
DOI: 10.48577/jpl.spuvpk
title: OCO-2/3 Calibration Report

description: No abstract available.
DOI: 10.48577/jpl.aqvdlm
title: Silicon Carbide and other wide bandgap semiconductors for optically and electrically readout magnetometry

description: No abstract available.
DOI: 10.48577/jpl.xajecx
title: Developing an Error Budget for GOMAP Studies

description: No abstract available.
DOI: 10.48577/jpl.japvct
title: Internal Electrostatic Assessment of Cables for PPE Module of Lunar Gateway

description: No abstract available.
DOI: 10.6084/m9.figshare.26490838
title: Data Set for A systematic review of figurational sociology within Physical Education research manuscript

description: Data Set for A systematic review of figurational sociology within Physical Education research manuscript
DOI: 10.6084/m9.figshare.26490838.v1
title: Data Set for A systematic review of figurational sociology within Physical Education research manuscript

description: Data Set for A systematic review of figurational sociology within Physical Education research manuscript
DOI: 10.48577/jpl.lrbr8w
title: ADVANCING SOIL MOISTURE ESTIMATION WITH ENHANCED SMAP ACTIVE/PASSIVE ALGORITHM FOR SMAP/NISAR COMBINED FRAMEWORK

description: No abstract available.
DOI: 10.48577/jpl.ucnzze
title: Overview: MEP Exploration Program and MEP Strategic Plan (NASA Town Hall Slides)

description: No abstract available.
DOI: 10.48577/jpl.fevzhs
title: History and Usage of a Figure of Merit for Injection Covariances

description: No abstract available.
DOI: 10.48577/jpl.sgcoyq
title: Getting Ready For NISAR Cryosphere Science Validation Using The NISAR On-Demand Cloud System

description: No abstract available.
DOI: 10.48577/jpl.8qx5ho
title: From Information to Knowledge and Back Again: How Information Management and Knowledge Management Work Together to Deliver Results

description: No abstract available.
DOI: 10.48577/jpl.rwgobc
title: Silicon Carbide and other wide bandgap semiconductors for optically and electrically readout magnetometry

description: No abstract available.
DOI: 10.48577/jpl.ojqrpu
title: I Put a Resonance Inside Your Resonance So You Can Overlap While You Overlap: Why 4th-Body Effects are Important in Multi-Moon Systems

description: No abstract available.
DOI: 10.48577/jpl.qq38mn
title: Large-eddy simulation (LES): a multi-purpose tool for atmospheric research and applications

description: No abstract available.
DOI: 10.48577/jpl.w0zwps
title: Endurance-A Development

description: No abstract available.
DOI: 10.48577/jpl.j1g9u4
title: Cosmology with Roman and Euclid

description: No abstract available.
DOI: 10.48577/jpl.uyhfjo
title: Europa Clipper Interplanetary Trajectory Navigation Analysis: General Results and Planetary Protection Strategy

description: No abstract available.
DOI: 10.48577/jpl.yxhd6y
title: SmallSat Presentation - LFL

description: No abstract available.
DOI: 10.48577/jpl.m8iefi
title: 4th Body-Induced Secondary Resonance Overlap Inside Normally Hyperbolic Invariant Manifolds in Planet-Moon Systems: a Jovian Case Study

description: No abstract available.
DOI: 10.48577/jpl.s2qi87
title: Leveraging VIPRE For End-To-End Trajectory And Science Optimization Of Outer Planet Probe Missions

description: No abstract available.
DOI: 10.5281/zenodo.13208449
title: Frankfurt /Main Apotheke Am Lindenbaum

description: Historical questionnaire/s 1924/1948 and index cards, partly selected enclosures regarding the history of a German pharmacy, catalogued via Kalliope portal (Historischer Fragebogen 1924/1948 und Karteikarten, ggf. gemeinfreie Anlagen zur Apothekengeschichte; als Katalog dient das Nachlassportal Kalliope): https://kalliope-verbund.info/DE-611-BF-70963 [Funktion: Im Findbuch anzeigen]Please note: The Kalliope catalogue entry might indicate related material in the archival folder which cannot be published due to copyright or other legal restrictions (NB: Das Katalogisat bei Kalliope kann auch auf Materialien - teils erheblichen Umfangs - verweisen, die aus archiv- oder urheberrechtlichen Gründen nicht veröffentlicht werden dürfen).
DOI: 10.48577/jpl.qo8p4h
title: Verifying SEFI Requirements for SOCs and Other Complex Devices

description: No abstract available.
DOI: 10.48577/jpl.o619pd
title: Exploring Mars Together: A Draft Plan for a Sustainable Future for Science at Mars

description: No abstract available.
DOI: 10.48577/jpl.1hshff
title: RISC-V and DDR4 SEETesting Update

description: No abstract available.
DOI: 10.48577/jpl.m7zeyc
title: 4th Body-Induced Secondary Resonance Overlap Inside Unstable Resonant Orbit Families: a Jupiter-Ganymede 4:3 + Europa Case Study

description: No abstract available.
DOI: 10.48577/jpl.fmeqrf
title: Towards a GPS High Accuracy Service (GPS HAS) Based on GDGPS and Related Applications

description: No abstract available.
DOI: 10.48577/jpl.bwhjq2
title: Promo Slide for Poster - Mars Sample Retrieval Lander Separation System: Key Challenges and Future Improvements

description: No abstract available.
DOI: 10.48577/jpl.pgstap
title: MAPPING AND CHARACTERIZING THE SOUTH POLAR DORSA ARGENTEA FORMATION USING THE MARSIS 3D VOLUME

description: No abstract available.
DOI: 10.48577/jpl.yakogu
title: Satellite Remote Sensing of Speciated Particulate Matter and Association with Adverse Health Effects in Europe as Part of Multi-Angle Imager for Aerosols (MAIA) Investigation

description: No abstract available.
DOI: 10.48577/jpl.cwyv74
title: Development of a Parabolic Reflector Radiator (PRR) for the LuSEE-Night Mission

description: No abstract available.
DOI: 10.48577/jpl.lhn73s
title: Endurance Mission-level Simulation Architecture for Autonomy Development

description: No abstract available.
DOI: 10.48577/jpl.ghjs8u
title: Thermal Analysis of Mars Orbital Sample Subsystem (OSS) for Sample Retrieval Lander

description: No abstract available.
DOI: 10.48577/jpl.nqiujf
title: Evolution of Antarctic Ozone, HCl, HNO3, ClO, and Related Species from MLS and WACCM (2004–2023)

description: No abstract available.
DOI: 10.48577/jpl.2ldmqt
title: What the Success of Spaceborne Optical Communications Means for the Future of Solar System Exploration

description: No abstract available.
DOI: 10.48577/jpl.akqthb
title: EXEP: Starshade Attributes

description: No abstract available.
DOI: 10.48577/jpl.ntbbt0
title: DUST AND LIFECYCLE TESTING OF COLDARM’S ACTUATORS FOR ANTICIPATED ENDURANCE-A REQUIREMENTS

description: No abstract available.
DOI: 10.48577/jpl.amdect
title: Calibration, Processing and Quality Assessment of NISAR L-band Level-1 and Level-2 Science Products

description: No abstract available.