E 1.99:nasa-tm--100894
|
Arc-textured metal surfaces for high thermal emittance space radiators |
1 |
E 1.99:nasa-tm--100946
|
Refractory metal alloys and composites for space power systems |
1 |
E 1.99:nasa-tm--101342
|
Materials technology assessment for a 1050 K Stirling Space Engine design |
1 |
E 1.99: nasa-tm--101364
|
Refractory metal alloys and composites for space nuclear power systems |
1 |
E 1.99:nasa-tm--101948
|
The emittance of space radiator materials measured at elevated temperatures |
1 |
E 1.99:nasa-tm--101956
|
Free-piston Stirling technology for space power |
1 |
E 1.99:nasa-tm--102044
|
Results from baseline tests of the SPRE I and comparison with code model predictions |
1 |
E 1.99:nasa-tm--102057
|
Two-dimensional numerical simulation of a Stirling engine heat exchanger |
1 |
E 1.99:nasa-tm--102059
|
CSTI high capacity power |
1 |
E 1.99:nasa-tm--102064
|
Space nuclear reactor shields for manned and unmanned applications |
1 |
E 1.99:nasa-tm--102322
|
Total hemispherical emittance measured at high temperatures by the calorimetric method |
1 |
E 1.99: nasa-tm--102390
|
Creep strength of niobium alloys, Nb-1%Zr and PWC-11 |
1 |
E 1.99:nasa-tm--103122
|
Recent Stirling engine loss - understanding results |
1 |
E 1.99:nasa-tm--103142
|
Programmatic status of NASÀ€s CSTI high capacity power Stirling Space Power Converter Program |
1 |
E 1.99:nasa-tm--103164
|
High frequency, high temperature specific core loss and dynamic B-H hysteresis loop characteristics of soft magnetic alloys |
1 |
E 1.99:nasa-tm--103168
|
Nuclear power systems for Lunar and Mars exploration |
1 |
E 1.99:nasa-tm--103203
|
The chemical effects of the Martian environment on power system component materials A theoretical approach. |
1 |
E 1.99:nasa-tm--103205
|
Aeolian removal of dust from radiator surfaces on Mars |
1 |
E 1.99:nasa-tm--103224
|
The effects of atomic oxygen on the thermal emittance of high temperature radiator surfaces |
1 |
E 1.99: nasa-tm--103612
|
Composite bearing and seal materials for advanced heat engine applications to 900 degree C |
1 |