3 edition of Cryogenic on-orbit liquid depot storage, acquisition, and transfer satellite (COLD-SAT) found in the catalog.
Cryogenic on-orbit liquid depot storage, acquisition, and transfer satellite (COLD-SAT)
by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC], [Springfield, Va
Written in English
|Statement||John R. Schuster and Edwin J. Russ and Joseph P. Wachter.|
|Series||NASA contractor report -- 185249., NASA contractor report -- NASA CR-185249.|
|Contributions||Russ, Edwin J., Wachter, Joseph P., United States. National Aeronautics and Space Administration.|
|The Physical Object|
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satellite data systems platforms experiments potential provide study requirements studies spacecraft skylab processing satellites launch design capability concept salyut You can write a book review and share your experiences. Other readers will. The On-Orbit Propellant Storage Stability investigation by Embry-Riddle Aeronautical University, Daytona Beach, Florida, continues a microgravity research program to determine stability data for a prototype orbiting fuel depot that could enable future long duration space missions.
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Full text of "Cryogenic On-Orbit Liquid Depot Storage, Acquisition, and Transfer Satellite (COLD-SAT)" See other formats. Get this from a library. Cryogenic on-orbit liquid depot storage, acquisition and transfer satellite (COLD-SAT) feasibility studies: final report. [W J Bailey; United. Get this from a library.
Feasibility study for a cryogenic on-orbit liquid depot-storage, acquisition and transfer (COLD-SAT) satellite: final report for phase A study, contract period, February - March [S C Rybak; United States. National Aeronautics and Space Administration.].
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 : William J.
Bailey. 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.
Four concurren studies, including one in-house at LeRC, are underway to determine the feasibility of performing model validation experiments aboard a free-flying spacecraft (S/C) called Cryogenic On-Orbit Liquid Depot — Storage, Acquisition and Transfer (COLD-SAT), using liquid hydrogen as the by: 1.
Cryogenic thermal system analysis for orbital propellant depot. transfer and filling of cryogenic liquid propellants require long-term storage, on-orbit fluid transfer and supply.
The design and requirements for the proposed cryogenic on-orbit liquid depot storage, acquisition, and transfer (COLD-SAT) satellite experiment, which is to be launched by Atlas I, are examined.
Thermal design considerations for the cryogenic on-orbit liquid depot storage, acquisition and transfer satellite (COLD-SAT) GRANT WILLIAMS and JOHN SCHUSTER. Jason William Hartwig, in Liquid Acquisition Devices for Advanced In-Space Cryogenic Propulsion Systems, Purpose of Work and Overview by Chapter.
The enabling of all future in-space cryogenic engines and cryogenic propellant depots for future manned and robotic space exploration missions begins with technology development of LADs upstream in the propellant tank.
The life of many instruments, laboratories and specialized satellite operating systems can be significantly extended if they are resupplied on orbit with superfluid helium. The resupply can take place from the Space Shuttle, from depot supply tanks at the space station or orbiting platform, or in-situ using the Orbital Maneuvering Vehicle (OMV Cited by: 2.
On orbit fuel depot: low boil off and in space 0g cryogenic fuel transfer ISRU: just about everything including - automated regolith / water ice handling in low gravity vacuum with large variation in temperature, high power generation & storage for two week night period; fuel transfer to cargo tanker on the lunar surface - all this in a dusty.
Cryogenic Fluid Management is a cross-cutting technology suite that supports multiple forms of propulsion systems (nuclear and chemical), including storage, transfer, and gauging, as well as liquefaction of ISRU (In-Situ Resource Utilization) produced propellants. Milestone B: Liquid oxygen storage of kg in a device under simulated LEO conditions (simulation of minute orbits) receiving a constantly interrupted power stream for LEO environment simulation purposes.
Winner: Lowest boil-off rate over one week. Milestone C: Liquid hydrogen storage of kg in a device under conditions of Milestone A. Macroeconomics is a branch of economics dealing with the performance, structure, behavior, and decision-making of an economy as a whole. This includes regional, national, and global economies.
Planetary or galactic. Some of it is about supplying services (like spacecraft rental or cargo shipping), some is about manufacturing, some is about resource development (mining), and some is about space.
Advances in in-space cryogenic fluid management technology can improve the affordability and performance of orbiting cryogenic propellant depots and hence the feasibility of long-duration exploration missions.
37 Research areas of particular interest include passive insulation and active cooling for zero boiloff; zero-gravity propellant. Unfortunately, this book can't be printed from the OpenBook. If you need to print pages from this book, we recommend downloading it as a PDF.
Visit to get more information about this book, to buy it in print, or to download it as a free PDF. Earth Station Facility Design Major Classes of Earth Stations TT&C Ground Facilities TV Uplinks and Broadcast Centers FDMA Digital Communications Service Full-Mesh TDMA Earth Station VSAT Star Network Terminal TV Receive-Only Design MSS User Terminals References CHAPTER 10 Launch Vehicles and.
data acquisition and documentation equipment: DADS: dual air density satellite: DAE: data acquisition equipment: DAF: data analysis facility: DAFT: data acquisition frequency table: DAI:. PDF; PDF; Print; Help NASA SBIR/STTR Program Support For questions about the NASA SBIR/STTR solicitations, the proposal preparation and electronic submission process, and other program related areas, please contact the NASA SBIR/STTR Program Support Office.
Phone: Email: [email protected] NASA SBIR/STTR Program Support is available Monday through Friday from. This subtopic seeks technologies related to cryogenic propellant (e.g.
hydrogen, oxygen, methane) production, storage, transfer, and usage to support NASA's in-situ resource utilization (ISRU) goals. This includes a wide range of applications, scales, and environments consistent with future NASA missions to the Moon and Mars.If successfully developed, a low weight cryogenic liquid generator could be applied to a cooling system for superconducting motor/generators, high powered jammers, and/or HEL type devices.
Metric goals and characteristics for the on-wing cryogenic liquid generator are as follows.26 27 The space shuttles main engines used liquid oxygen and liquid hydrogen that were pumped from the launch pads ground storage units into the external fuel tank.
During the Space Shuttle Program, it took many people to operate and maintain the cryogenic loading system, said Barbara Brown, a project manager in NASAs Engineering and Technology.