Data management study, volume 5. Appendix K - Contractor data package data management /DM/ Final report
Contractor data management system for Voyager project
DATA HANDLING SYSTEM↗
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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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Packaging data products using data grid middleware for Deep Space Mission Systems
We are investigating a distributed computing infrastructure for releasing science products out of the mission pipeline. We are creating a DSMS Product Service and DSMS Data Packaging Service based on the OODT middleware, a Data Grid middleware technology that has proven successful in providing access to heterogeneous, disparate data, and federating that data using a common data model.
Deep Space Mission Systems↗
Long duration exposure facility solar illumination data package
A post flight solar illumination data package was created by the LDEF thermal analysis data group in support of the LDEF science office data group. The data presented was prepared with the Thermal Radiation Analysis System (TRASYS) program. Ground tracking data was used to calculate daily orbital beta angles for the calculation of resultant fluxes. This data package will be useful in calculation of solar illumination fluent for a variety of beta angle orbital conditions encountered during the LDEF mission.
Berrios, William M.↗
Thematic mapper flight model preshipment review data package. Volume 4: Appendix. Part C: Power supply data
The acceptance test data package for the thematic mapper flight model power supply was reviewed and the data compared to the relevant specification. The power supply was found to be within specification. Final test data for outut voltage regulation and ripple, efficiency, over and undervoltage protection, telemetry, impedances, turn-on requirements, and input current limits are presented.
Source record↗
Preparing safety data packages for experimenters using the Get Away Special (GAS) carrier system
The implementation of NSTS 1700.7B and more forceful scruntiny of data packages by the Johnson Space Flight Center (JSC) lead to the development of a classification policy for GAS/CAP payloads. The purpose of this policy is to classify experiments using the carrier system so that they receive an appropriate level of JSC review (i.e., one or multiphase reviews). This policy is based on energy containment to show inherent payload safety. It impacts the approach to performing hazard analyses and the nature of the data package. This paper endeavors to explain the impact of this policy as well as the impact of recent JSC as well as Kennedy Space Flight Center (KSC) 'interpretations' of existing requirements. The GAS canister does adequately contain most experiments when flown in the sealed configuration (however this must be shown, not merely stated). This paper also includes data package preparation guidelines for those experiments that require an opening door which often present unique safety issues.
Kosko, Jerome↗
Data management study, volume 5. Appendix D - Contractor data package configuration management /CM/ Final report
Contractor data package for Voyager spacecraft configuration management
SPACECRAFT CONFIGURATION↗
JPL's End Item Data Packages (EIDPs)
A viewgraph presentation on JPL's End Item Data Packages (EIDPs) is shown. The topics include: 1) Background and past efforts; 2) Current effort; and 3) First look; 4) Final look; and 5) Next steps.
End Item Data Package (EIDP)↗
Data Management Study, Volume 5. Appendix H - Contractor Data Package Logistics and Support /LS/ Final Report
Contractor data package for Voyager logistics and support in transportation, communications, supply, and maintenance
SUPPORT SYSTEM↗
Data management study, volume 5. Appendix J - Contractor data package procurement and contracting /PC/ Final report
Contractor data package for administration of procurement and contracting of Voyager spacecraft systems
VOYAGER PROJECT↗
Thematic mapper flight model preshipment review data package. Volume 2, part A: Subsystem data
Performance and acceptance data are presented for the multiplexer, scan mirror, power supply, mainframe/top mechanical and the aft optics, assemblies. Other major subsystems evaluated include the relay optics, the electronic module, the radiative cooler, and the cable harness. Reference lists of nonconforming materials reports, failure reports, and requests for deviation/waiver are also given.
Source record↗
Thematic mapper flight model preshipment review data package. Volume 2, part B: Subsystem data
Summarized performance data are presented for the following major subsystems of the thematic mapper: the focal plane assembly, the radiative cooler, the radiative cooler door assembly, the top optical assembly, and the telescope assembly. Reference lists of the configurations status and of nonconforming material reports, failure reports, and requests for deviation/waiver are included.
Source record↗
Thematic mapper flight model preshipment review data package. Volume 2, part C: Subsystem data
Reference lists are provided to acceptance data for each of the major subsystems of the thematic mapper. Configuration reports, lists and copies of all failure reports, and requests for deviation/waiver are included.
Source record↗
Thematic mapper flight model preshipment review data package. Volume 3, part A: System data
Results of vibration, acoustical noise, and thermal vacuum are described as well as tests studies of EMI/EMC and mass properties conducted for thematic mapper systems integration. Liens are summarized and the engineering change proposal status is presented. Requests for deviation/waiver are included along with failure and nonforming material reports.
Source record↗
Thematic mapper flight model preshipment review data package. Volume 3, part B: System data
Procedures and results are presented for performance and systems integration tests of flight model-1 thematic mapper. Aspects considered cover electronic module integration, radiometric calibration, spectral matching, spatial coverage, radiometric calibration of the calibrator, coherent noise, dynamic square wave response, band to band registration, geometric accuracy, and self induced vibration. Thermal vacuum tests, EMI/EMS, and mass properties are included. Liens are summarized.
Source record↗
Thematic mapper flight model preshipment review data package. Volume 3, part C: System data
Failure reports for flight model-1 of the thematic mapper are summarized showing the symptom and cause of failure as well as the corrective action taken. Each report is keyed to the major subsystem against which the failure occurred. Requests for deviation/waiver are listed by number, description, and current status. Copies of engineering proposals are included.
Source record↗
Data management study, volume 5. Appendix F - Contractor data package test /TE/ and mission operations /MP/ Final report
Test and mission operations contractor data package for Voyager spacecraft
VOYAGER PROJECT↗
Acceptance Data Package: SXI Stepper Motor/Encoder. Aeroflex P/N 16187: Engineering Drawings and Associated Lists - A
Acceptance data package - engineering drawings and associated lists for fabrication, assembly and maintenance (cleaning, fluidized bed coating, bounding and staking) motor/encoded solar x-ray imager (SXI) (Aeroflex p/n 16187) were given.
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Preliminary design data package, appendix C
The data and documentation required to define the preliminary design of a near term hybrid vehicle and to quantify its operational characteristics are presented together with the assumptions and rationale behind the design decisions. Aspects discussed include development requirements for the propulsion system, the chassis system, the body, and the vehicle systems. Particular emphasis is given to the controls, the heat engine, and the batteries.
Source record↗