Cryogenic On-orbit Liquid Depot Storage Acquisition and Transfer (COLD-SAT) Experiment Subsystem Instrumentation and Wire Harness Design Report

Cryogenic On-orbit Liquid Depot Storage Acquisition and Transfer (COLD-SAT) Experiment Subsystem Instrumentation and Wire Harness Design Report PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 76

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 956

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Cryogenic On-Orbit Liquid Depot Storage Acquisition and Transfer (Cold-Sat) Experiment Subsystem Instrumentation and Wire Harness Design Report

Cryogenic On-Orbit Liquid Depot Storage Acquisition and Transfer (Cold-Sat) Experiment Subsystem Instrumentation and Wire Harness Design Report PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722330156
Category :
Languages : en
Pages : 74

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Subcritical cryogens such as liquid hydrogen (LH2) and liquid oxygen (LO2) are required for space based transportation propellant, reactant, and life support systems. Future long-duration space missions will require on-orbit systems capable of long-term cryogen storage and efficient fluid transfer capabilities. COLD-SAT, which stands for cryogenic orbiting liquid depot-storage acquisition and transfer, is a free-flying liquid hydrogen management flight experiment. Experiments to determine optimum methods of fluid storage and transfer will be performed on the COLD-SAT mission. The success of the mission is directly related to the type and accuracy of measurements made. The instrumentation and measurement techniques used are therefore critical to the success of the mission. This paper presents the results of the COLD-SAT experiment subsystem instrumentation and wire harness design effort. Candidate transducers capable of fulfilling the COLD-SAT experiment measurement requirements are identified. Signal conditioning techniques, data acquisition requirements, and measurement uncertainty analysis are presented. Electrical harnessing materials and wiring techniques for the instrumentation designed to minimize heat conduction to the cryogenic tanks and provide optimum measurement accuracy are listed. Edwards, Lawrence G. Unspecified Center...

Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1100

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1994

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Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 616

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Government Reports Annual Index

Government Reports Annual Index PDF Author:
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Category : Government publications
Languages : en
Pages : 1224

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Cryogenic On-Orbit Liquid Depot Storage, Acquisition, and Transfer Satellite (Cold-Sat) Feasibility Study

Cryogenic On-Orbit Liquid Depot Storage, Acquisition, and Transfer Satellite (Cold-Sat) Feasibility Study PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723549816
Category :
Languages : en
Pages : 328

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The Cryogenic On-Orbit Liquid Depot Storage, Acquisition, and Transfer Satellite (COLD-SAT) is an experimental spacecraft launched from an expendable launch vehicle which is designed to investigate the systems and technologies required for efficient, effective, and reliable management of cryogenic fluid in the reduced gravity space environment. The COLD-SAT program will provide the necessary data base and provide low-g proving of fluid and thermal models of cryogenic storage, transfer, and resupply concepts and processes. A conceptual approach was developed and an overview of the results of the 24 month COLD-SAT Phase A feasibility is described which includes: (1) a definition of the technology needs and the accompanying experimental 3 month baseline mission; (2) a description of the experiment subsystem, major features and rationale for satisfaction of primary and secondary experiment requirements using liquid hydrogen as the test fluid; and (3) a presentation of the conceptual design of the COLD-SAT spacecraft subsystems which support the on-orbit experiment with emphasis on areas of greatest challenge. Bailey, William J. and Weiner, Stephen P. and Beekman, Douglas H. and Dennis, Mark F. and Martin, Timothy A. Unspecified Center NASA-CR-185247, NAS 1.26:185247, MCR-90-1307 NAS3-25063; RTOP 506-48-21...

Cryogenic On-Orbit Liquid Depot-Storage, Acquisition and Transfer (Cold-Sat) Experiment Conceptual Design and Feasibility Study

Cryogenic On-Orbit Liquid Depot-Storage, Acquisition and Transfer (Cold-Sat) Experiment Conceptual Design and Feasibility Study PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723549854
Category :
Languages : en
Pages : 596

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The cryogenic fluid management technologies required for the exploration of the solar system can only be fully developed via space-based experiments. A dedicated spacecraft is the most efficient way to perform these experiments. This report documents the extended conceptual design of the COLD-SAT spacecraft, capable of meeting these experimental requirements. All elements, including the spacecraft, ground segment, launch site modifications and launch vehicle operations, and flight operations are included. Greatly expanded coverage is provided for those areas unique to this cryogenic spacecraft, such as the experiment system, attitude control system, and spacecraft operations. Supporting analyses are included as are testing requirements, facilities surveys, and proposed project timelines. Kramer, Edward (Editor) Glenn Research Center NASA/TP-1998-3523, NAS 1.60:3523, E-9130 RTOP 506-48-00...

Guidelines and Metrics for Assessing Space System Cost Estimates

Guidelines and Metrics for Assessing Space System Cost Estimates PDF Author: Bernard Fox
Publisher: RAND Corporation
ISBN:
Category : History
Languages : en
Pages : 268

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1. Introduction / 2. Space system fundamentals / 3. Reviewing a cost estimate / 4. Space vehicle cost crosschecks / 5. Common issues in estimating space programs / 6. Resources for space system cost estimation / 7. Recommendations.