The Thermal Energy Storage-1 (TES-1) is a flight experiment that flew on the Space Shuttle Columbia (STS-62), in March 1994, as part of the OAST-2 mission. TES-1 is the first experiment in a four experiment suite designed to provide data for understanding the long duration microgravity behavior of thermal energy storage fluoride salts that undergo repeated melting and freezing. Such data have never been obtained before and have direct application for the development of space-based solar dynamic (SD) power systems. These power systems will store solar energy in a thermal energy salt such as lithium fluoride or calcium fluoride. The stored energy is extracted during the shade portion of the orbit. This enables the solar dynamic power system t...
The development of a modular solar thermal power system for application in the 1 to 10 MWe range is ...
The testing of a full-size, 120 kW, solar dynamic heat receiver utilizing high-temperature thermal e...
A heatpipe experiment for a long duration exposure facility is described. The design and configurati...
A 16 parameter solar concentrator/heat receiver mass model is used in conjunction with Stirling and ...
Spacecraft solar dynamic power systems typically use high-temperature phase-change materials to effi...
Thermal energy storage materials for use in solar thermionic power spacecraft system
The structural performance of a space station thermal energy storage (TES) canister subject to orbit...
A long term mission in a lunar base presents technological challenges that have not been solved yet...
Thermophysical properties of potential thermal energy storage materials for design of TES THERMIONIC...
The Solar Dynamic Power Module being developed for Space Station Freedom uses a eutectic mixture of ...
Thermal Energy Storage (TES) is one of the techniques that can be used to store the solar energy for...
The general scope of study on thermal energy storage development includes: (1) survey and review po...
A long term mission in a lunar base presents technological challenges that have not been solved yet....
The Space Experiments Division at NASA Lewis Research Center is developing technology and science sp...
Advanced energy storage and power management systems designed through rigorous materials selection, ...
The development of a modular solar thermal power system for application in the 1 to 10 MWe range is ...
The testing of a full-size, 120 kW, solar dynamic heat receiver utilizing high-temperature thermal e...
A heatpipe experiment for a long duration exposure facility is described. The design and configurati...
A 16 parameter solar concentrator/heat receiver mass model is used in conjunction with Stirling and ...
Spacecraft solar dynamic power systems typically use high-temperature phase-change materials to effi...
Thermal energy storage materials for use in solar thermionic power spacecraft system
The structural performance of a space station thermal energy storage (TES) canister subject to orbit...
A long term mission in a lunar base presents technological challenges that have not been solved yet...
Thermophysical properties of potential thermal energy storage materials for design of TES THERMIONIC...
The Solar Dynamic Power Module being developed for Space Station Freedom uses a eutectic mixture of ...
Thermal Energy Storage (TES) is one of the techniques that can be used to store the solar energy for...
The general scope of study on thermal energy storage development includes: (1) survey and review po...
A long term mission in a lunar base presents technological challenges that have not been solved yet....
The Space Experiments Division at NASA Lewis Research Center is developing technology and science sp...
Advanced energy storage and power management systems designed through rigorous materials selection, ...
The development of a modular solar thermal power system for application in the 1 to 10 MWe range is ...
The testing of a full-size, 120 kW, solar dynamic heat receiver utilizing high-temperature thermal e...
A heatpipe experiment for a long duration exposure facility is described. The design and configurati...