Stack tests indicate that the discrepancies between calculated and measured temperature profiles are due to reactant cross-over and a lower than expected thermal conductivity of cells. Preliminary results indicate that acceptable contact resistance between cooling plane halves can be achieved without the use of paper. The preliminary design of the enclosure, definition of required labor and equipment for manufacturing repeating components, and the assembly procedures for the benchwork design were developed. Fabrication of components for a second 5-cell stack of the MK-2 design and a second 23-cell stack of the MK-1 design was started. The definition of water and fuel for the reforming subsystem was developed along with a preliminary definit...
NASA LeRC is currently developing a FORTRAN based computer model of a complete nuclear electric prop...
This report summarizes the work performed for Phase I (October 2001 - August 2006) under Cooperative...
An opposed reacting jet combustor (ORJ) was tested at a pressure of 1 atmosphere. A premixed propane...
The results of the completed tests on Stack 561 and the on-going tests of 562 (23 cell stacks of the...
The design features and plans for fabrication of Stacks 564 and 800 are described. The results of th...
abstract: Determining the thermal conductivity of carbon gas diffusion layers used in hydrogen fuel ...
The work performed during the Second Logical Unit of Work of a multi-year program designed to develo...
First conceived in the 1940s, nuclear thermal propulsion (NTP) is a viable and advantageous method o...
An engineered thick thermal barrier coating consisting of multiple layers of zirconia and CoCrAlY wi...
Two 25 cell stacks of the 13 inch x 23 inch cell size (about 4kW) remain on test after 4000 hours an...
The design and development of eight prototype solar heating and combined heating and cooling systems...
The MSFC solar heating and cooling facility was assembled to demonstrate the engineering feasibility...
The results of a materials technology program for a long-life (50,000 hr), high-temperature (950 C c...
Work on heat transport fluids for use with active solar heating and cooling systems is described. Pr...
Conceptual designs for radioisotope heat source systems to provide 25 kW thermal power to Brayton cy...
NASA LeRC is currently developing a FORTRAN based computer model of a complete nuclear electric prop...
This report summarizes the work performed for Phase I (October 2001 - August 2006) under Cooperative...
An opposed reacting jet combustor (ORJ) was tested at a pressure of 1 atmosphere. A premixed propane...
The results of the completed tests on Stack 561 and the on-going tests of 562 (23 cell stacks of the...
The design features and plans for fabrication of Stacks 564 and 800 are described. The results of th...
abstract: Determining the thermal conductivity of carbon gas diffusion layers used in hydrogen fuel ...
The work performed during the Second Logical Unit of Work of a multi-year program designed to develo...
First conceived in the 1940s, nuclear thermal propulsion (NTP) is a viable and advantageous method o...
An engineered thick thermal barrier coating consisting of multiple layers of zirconia and CoCrAlY wi...
Two 25 cell stacks of the 13 inch x 23 inch cell size (about 4kW) remain on test after 4000 hours an...
The design and development of eight prototype solar heating and combined heating and cooling systems...
The MSFC solar heating and cooling facility was assembled to demonstrate the engineering feasibility...
The results of a materials technology program for a long-life (50,000 hr), high-temperature (950 C c...
Work on heat transport fluids for use with active solar heating and cooling systems is described. Pr...
Conceptual designs for radioisotope heat source systems to provide 25 kW thermal power to Brayton cy...
NASA LeRC is currently developing a FORTRAN based computer model of a complete nuclear electric prop...
This report summarizes the work performed for Phase I (October 2001 - August 2006) under Cooperative...
An opposed reacting jet combustor (ORJ) was tested at a pressure of 1 atmosphere. A premixed propane...