A 1.2- by 1.8-m variable conductance heat pipe radiator was designed, built, and tested. The radiator has deployment capability and can passively control Freon-21 fluid loop temperatures under varying loads and environments. It consists of six grooved variable conductance heat pipes attached to a 0.032-in. aluminum panel. Heat is supplied to the radiator via a fluid header or a single-fluid flexible heat pipe header. The heat pipe header is an artery design that has a flexible section capable of bending up to 90 degrees. Radiator loads as high as 850 watts were successfully tested. Over a load variation of 200 watts, the outlet temperature of the Freon-21 fluid varied by 7 F. An alternate control system was also investigated which used a v...
Bellows, metallic diaphragm, and paddle vortex subcritical transfer systems designs and high pressur...
Heat pipe manufacturing methods are examined with the goal of establishing cost effective procedures...
An apparatus is described which can deliver uniform heat flux densities of up to 80 W/sq cm over an ...
A 15,000 watt spacecraft waste heat rejection system utilizing heat pipe radiator panels was investi...
Continuing efforts in large gains in heat-pipe performance are reported. It was found that gas-contr...
The construction and operational characteristics of an extended life flexible radiator panel is desc...
Analysis of the data heat pipe radiator systems tested in both vacuum and ambient environments was c...
A full scale prototype flexible radiator panel was designed, built and tested. The panel, has approx...
The results of a thermal-structural test program to verify the performance of a metallic/radiative T...
The development of spiral artery cryogenic thermal diode heat pipes was continued. Ethane was the wo...
An optimized flight-weight prototype fluid-header panel (heatpipe radiator system) was tested in a v...
A collector/heat pipe cooled, externally configured (heated) thermionic diode module was designed fo...
A description is given of the design approach followed and the results of the analysis leading up to...
The Redesigned Solid Rocket Motors (RSRM) of the Space Transportation System have three field joints...
The soft tube radiator subsystem is described including applicable system requirements, the design a...
Bellows, metallic diaphragm, and paddle vortex subcritical transfer systems designs and high pressur...
Heat pipe manufacturing methods are examined with the goal of establishing cost effective procedures...
An apparatus is described which can deliver uniform heat flux densities of up to 80 W/sq cm over an ...
A 15,000 watt spacecraft waste heat rejection system utilizing heat pipe radiator panels was investi...
Continuing efforts in large gains in heat-pipe performance are reported. It was found that gas-contr...
The construction and operational characteristics of an extended life flexible radiator panel is desc...
Analysis of the data heat pipe radiator systems tested in both vacuum and ambient environments was c...
A full scale prototype flexible radiator panel was designed, built and tested. The panel, has approx...
The results of a thermal-structural test program to verify the performance of a metallic/radiative T...
The development of spiral artery cryogenic thermal diode heat pipes was continued. Ethane was the wo...
An optimized flight-weight prototype fluid-header panel (heatpipe radiator system) was tested in a v...
A collector/heat pipe cooled, externally configured (heated) thermionic diode module was designed fo...
A description is given of the design approach followed and the results of the analysis leading up to...
The Redesigned Solid Rocket Motors (RSRM) of the Space Transportation System have three field joints...
The soft tube radiator subsystem is described including applicable system requirements, the design a...
Bellows, metallic diaphragm, and paddle vortex subcritical transfer systems designs and high pressur...
Heat pipe manufacturing methods are examined with the goal of establishing cost effective procedures...
An apparatus is described which can deliver uniform heat flux densities of up to 80 W/sq cm over an ...