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

Download or read book Cryogenic On Orbit Liquid Depot Storage Acquisition and Transfer Cold Sat Experiment Subsystem Instrumentation and Wire Harness Design Report written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-08 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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...

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

Download or read book Cryogenic On orbit Liquid Depot Storage Acquisition and Transfer COLD SAT Experiment Subsystem Instrumentation and Wire Harness Design Report written by and published by . This book was released on 1994 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 956 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Cryogenic On Orbit Liquid Depot Storage  Acquisition  and Transfer Satellite  Cold Sat  Feasibility Study

Download or read book Cryogenic On Orbit Liquid Depot Storage Acquisition and Transfer Satellite Cold Sat Feasibility Study written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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...

Book Cryogenic On Orbit Liquid Depot Storage  Acquisition and Transfer  Cold Sat  Experiment Conceptual Design and Feasibility Study

Download or read book Cryogenic On Orbit Liquid Depot Storage Acquisition and Transfer Cold Sat Experiment Conceptual Design and Feasibility Study written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 596 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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...

Book Cryogenic On Orbit Liquid Depot Storage  Acquisition  and Transfer Satellite  Cold Sat

Download or read book Cryogenic On Orbit Liquid Depot Storage Acquisition and Transfer Satellite Cold Sat written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Cryogenic On-Orbit Liquid Depot Storage, Acquisition, and Transfer Satellite (COLD-SAT) will perform subcritical liquid hydrogen handling experiments under low gravity conditions to provide engineering data for future space transportation missions. Comprising the four Class 1 enabling experiments are tank press control, tank chilldown, tank no-vent fill, and liquid acquisition device fill/refill. The nine Class 2 enhancing experiments are tanker thermal performance, pressurization, low-gravity setting and outflow, liquid acquisition device performance, transfer line chilldown, outflow subcooling, low-gravity vented fill, fluid dumping, and advanced instrumentation. Consisting of an experiment module mated to a spacecraft bus, COLD-SAT will be placed in an initial 1300 km circular orbit by an Atlas commercial launch vehicle, and will perform experiments in a semi-autonomous mode for a period of up to six months. The three-axis controlled spacecraft bus provides electric power, control and data management, communications, and attitude control along with propulsive acceleration levels ranging from 10(exp -6) to 10(exp -4) g. It is desired to understand the effects that low acceleration levels might have on the heat and mass transfer processes involved in some of the experiments. The experiment module contains the three liquid hydrogen tanks, valves, pressurization and pumping equipment, and instrumentation. Within the highly insulated tanks are specialized fluid management equipment that might be used in future space transportation systems. At launch all the liquid hydrogen for the experiments is contained in the largest tank, which has helium-purged insulation to prevent cryo-pumping of air on the launch pad. The tank is loaded by the hydrogen tanking system used for the Centaur upper stage of the Atlas. After reaching orbit the two smaller tanks become receivers for fluid transfers, and when tanked, become the vessels for performing many of the experiments. Schus...

Book CRYOGENIC ON ORBIT LIQUID DEPOT STORAGE  ACQUISITION AND TRANSFER  COLD SAT  EXPERIMENT CONCEPTUAL DESIGN AND    NASA TP 1998 3523    MAR  1

Download or read book CRYOGENIC ON ORBIT LIQUID DEPOT STORAGE ACQUISITION AND TRANSFER COLD SAT EXPERIMENT CONCEPTUAL DESIGN AND NASA TP 1998 3523 MAR 1 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1999* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly Catalogue  United States Public Documents

Download or read book Monthly Catalogue United States Public Documents written by and published by . This book was released on 1995 with total page 1100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Feasibility Study for a Cryogenic On Orbit Liquid Depot Storage  Acquisition and Transfer  Cold Sat  Satellite

Download or read book Feasibility Study for a Cryogenic On Orbit Liquid Depot Storage Acquisition and Transfer Cold Sat Satellite written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt: This feasibility study presents the conceptual design of a spacecraft for performing a series of cryogenic fluid management flight experiments. This spacecraft, the Cryogenic On-Orbit Liquid Depot-Storage, Acquisition, and Transfer (COLD-SAT) satellite, will use liquid hydrogen as the test fluid, be launched on a Delta expendable launch vehicle, and conduct a series of experiments over a two to three month period. These experiments will investigate the physics of subcritical cryogens in the low gravity space environment to characterize their behavior and to correlate the data with analytical and numerical models of in-space cryogenic fluid management systems. Primary technologies addressed by COLD-SAT are: (1) pressure control; (2) chilldown; (3) no-vent fill; (4) liquid acquisition device fill; (5) pressurization; (6) low-g fill and drain; (7) liquid acquisition device expulsion; (8) line chilldown; (9) thermodynamic state control; and (10) fluid dumping. Rybak, S. C. and Willen, G. S. and Follett, W. H. and Hanna, G. J. and Cady, E. C. and Distefano, E. and Meserole, J. S. Unspecified Center NASA-CR-185248, NAS 1.26:185248 NAS3-25054...

Book COLD SAT

    Book Details:
  • Author :
  • Publisher :
  • Release : 1989
  • ISBN :
  • Pages : pages

Download or read book COLD SAT written by and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Government Reports Announcements   Index

Download or read book Government Reports Announcements Index written by and published by . This book was released on 1994 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Government Reports Annual Index

Download or read book Government Reports Annual Index written by and published by . This book was released on 1994 with total page 1224 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Cold SAT

    Book Details:
  • Author : National Aeronautics and Space Administration (NASA)
  • Publisher : Createspace Independent Publishing Platform
  • Release : 2018-08-16
  • ISBN : 9781725572140
  • Pages : 30 pages

Download or read book Cold SAT written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-16 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: The COLD-SAT spacecraft will perform subcritical liquid hydrogen storage and transfer experiments under low-gravity conditions to provide engineering data for future space transportation missions. Consisting of an experiment module mated to a spacecraft bus, COLD-SAT will be placed in an initial 460 km circular orbit by an Atlas I commercial launch vehicle. After deployment, the three-axis-controlled spacecraft bus will provide electric power, experiment control and data management, communications, and attitude control along with propulsive acceleration levels ranging from 10(-6) to 10(-4)g. These accelerations are an important aspect of some of the experiments, as it is desired to know the effects that low gravity levels might have on the heat and mass transfer processes involved. The experiment module will contain the three liquid hydrogen tanks, valves, pressurization equipment, and instrumentation. At launch all the hydrogen will be in the largest tank, which has helium-purged MLI and is loaded and topped off by the hydrogen tanking system used for the Centaur upper stage of the Atlas. The two smaller tanks will be utilized in orbit for performing some of the experiments. The experiments are grouped into two classes on the basis of their priority, and include six regarded as enabling technology and nine regarded as enhancing technology. Schuster, J. R. and Wachter, Joseph P. and Powers, Albert G. Glenn Research Center NASA-TM-102303, E-4984, NAS 1.15:102303, IAF-89-057 RTOP 506-48-21...

Book Large Scale Cryogenic Fluid Systems Testing

Download or read book Large Scale Cryogenic Fluid Systems Testing written by and published by . This book was released on 1992 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Conceptual Design and Analysis of Orbital Cryogenic Liquid Storage and Supply Systems

Download or read book Conceptual Design and Analysis of Orbital Cryogenic Liquid Storage and Supply Systems written by Ralph N. Eberhardt and published by . This book was released on 1981 with total page 205 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wide variety of orbital cryogenic liquid storage and supply systems are defined in NASA and DOD long-range plans. These systems include small cooling applications, large chemical and electrical orbit transfer vehicles and resupply tankers. All have the common requirements of low-g fluid management to accomplish gas-free liquid expulsion and efficient thermal control to manage heat leak and tank pressure. A preliminary design study was performed to evaluate tanks ranging from 0.6 to 37.4 cu. 3 (22 to 1320 cu. ft). Liquids of interest were hydrogen, oxygen, methane, argon and helium. Conceptual designs were generated for each tank system and fluid dynamic, thermal and structural analyses were performed for Shuttle compatible operations. Design trades considered the paradox of conservative support structure and minimum thermal input. Orbital performance and weight data were developed, and a technology evaluation was completed. (Author).

Book Guidelines and Metrics for Assessing Space System Cost Estimates

Download or read book Guidelines and Metrics for Assessing Space System Cost Estimates written by Bernard Fox and published by RAND Corporation. This book was released on 2008 with total page 268 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.