The JPL Open Repository (JOR) replaced the JPL Technical Report Server (TRS) in 2023. It is a repository for digital copies of technical publications authored by JPL employees. It includes journal articles (the Final Accepted Version), meeting papers, presentations, and other publications cleared for external distribution from 1992 to the present. It also includes research datasets from 2022 on.

Years covered: 1992 to the present.
  • 1992-2021 records were originally on the JPL Technical Report Server (TRS) on Dspace system; those records were migrated to Dataverse in 2022.
  • Records with publication date 2022 or later are native to the Dataverse.
  • Data sets: 2022 to present
  • There are a few pre-1992 records. Those were added to the system on a case-by-case request basis.

  • Persistent IDs (PIDs):
  • 1992-2021 records have Handles
  • 2022 and later records have Digital Object Identifiers (DOIs).
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    83,951 to 83,960 of 84,733 Results
    Lambda-Point Experimant Helium Cryostat Cryoservicing, Functions, and Performance
    Jul 1, 1993
    Petrac, D.; Israelsson, U. E.; Luchik, T. S., 1993, "Lambda-Point Experimant Helium Cryostat Cryoservicing, Functions, and Performance", https://hdl.handle.net/2014/34841, Alburquerque, New Mexico, USA, JPL Open Repository
    No abstract provided
    Time Parallel Solution of Linear Partial Differential Equations on the Intel Touchstone Delta Supercomputer
    Jul 1, 1993
    Toomarian, N.; Fijany, A.; Barhen, J., 1993, "Time Parallel Solution of Linear Partial Differential Equations on the Intel Touchstone Delta Supercomputer", https://hdl.handle.net/2014/35639, Concurrency, JPL Open Repository
    Evolutionary partial differential equations are usually solved by decretization in time and space, and by applying a marching in time procedure to data and algorithms potentially parallelized in the spatial domain.
    Meeting with a Majestic Giant: The Cassini Mission to Saturn
    Jul 1, 1993
    Kohlhase, C., 1993, "Meeting with a Majestic Giant: The Cassini Mission to Saturn", https://hdl.handle.net/2014/35742, Planetary Report, JPL Open Repository
    In October of 1997, a two-story-tall robotic spacecraft will begin a journey of many years to the vast and exiting realm of Saturn. With a mass of roughly 2,500 kilograms (5,510 pounds) of dry hardware and 3,000 kilograms (6,615 pounds) of propellant, it needs a boost from the Ti...
    Large Doping-Spike PtSi LWIR Focal Plane Arrays for Astronomy
    Jul 1, 1993
    Lin, T. L.; Park, J. S.; Gunapala, S.; Jones, E. W.; DelCastillo, H. M.; Herring, J., 1993, "Large Doping-Spike PtSi LWIR Focal Plane Arrays for Astronomy", https://hdl.handle.net/2014/35355, Los Angeles, California, USA, JPL Open Repository
    No abstract provided
    Compensation for the Atmosphere in Radiance Measured by the Airborne Visible/Infrared Imaging Spectrometer and Applications to an Advanced Land Remote Sensing System
    Jun 29, 1993
    Green, R. O.; Conel, J. E., 1993, "Compensation for the Atmosphere in Radiance Measured by the Airborne Visible/Infrared Imaging Spectrometer and Applications to an Advanced Land Remote Sensing System", https://hdl.handle.net/2014/35729, Torrance, California, USA, JPL Open Repository
    The Airborne Visible/Infrared Imaging Spectrometer measures spatial images of the total upwelling spectral radiance from 400 to 2500 nm through 10 nm spectral channels. Quantitative research and application objectives for surface investigations require conversion of the measured...
    Initial Galileo Propulsion System In-Flight Characterization
    Jun 28, 1993
    Barber, T.J.; Krug, F.A.; Froidevaux, B.M., 1993, "Initial Galileo Propulsion System In-Flight Characterization", https://hdl.handle.net/2014/35187, Monterey, California, USA, JPL Open Repository
    The Galileo RetroPropulsion Module (RPM) has performed excellently throughout the first three years of mission operations. The RPM is a state-of-the-art, pressure-fed, bipropellant propulsion system, provided to NASA by the Federal Republic of Germany.
    Hybrid Propulsion Based on Fluid-Controlled Solid Gas Generators
    Jun 28, 1993
    Cohen, Norman S.; Strand, Leon D., 1993, "Hybrid Propulsion Based on Fluid-Controlled Solid Gas Generators", https://hdl.handle.net/2014/35344, Monterey, California, USA, JPL Open Repository
    The use of fuel-rich solid (gas generator-type) propellants for hybrid propulsion affords some design and utilization efficiency advantages. Both forward and aft liquid injection control concepts are evaluated form the operational standpoints of ballistics, throttling, Stability...
    Mars Observer PMIRR: Applications to Atmospheric Transport
    Jun 28, 1993
    R.W. Zurek; McCleese, D.J., 1993, "Mars Observer PMIRR: Applications to Atmospheric Transport", https://hdl.handle.net/2014/35242, Corvallis, Oregon State, USA, JPL Open Repository
    No abstract provided
    Hybrid Rocket Combustion Study
    Jun 28, 1993
    Strand, L.D.; Ray, R.L.; Cohen, N.S., 1993, "Hybrid Rocket Combustion Study", https://hdl.handle.net/2014/35490, Monterey, California, USA, JPL Open Repository
    The objectives of this study of
    Evidence for Dust Transport In Viking IR Thermal Mapper Opacity Data
    Jun 28, 1993
    Martin, T. Z., 1993, "Evidence for Dust Transport In Viking IR Thermal Mapper Opacity Data", https://hdl.handle.net/2014/35203, Oregon, USA, JPL Open Repository
    No abstract provided
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