Add to ORKGA series of six heat pipes, similar in design to those flown on the Comunications Technology Satellite Hermes, for use in a prototype Solar Electric Propulsion BIMOD thrust module are evaluated. The results of acceptance and characterization tests performed on the heat pipe subassemble are reported. The performance of all the heat pipes met, or exceeded, design specifications
This report covers the design, fabrication, and test of several dual slot heat pipe engineering deve...
The OAO-C spacecraft has three circular heat pipes, each of a different internal design, located in ...
Various heat pipe temperature control techniques are critically evaluated using characteristic featu...
As part of an effort to develop reliable, cost effective spacecraft thermal control heat pipes, life...
Development in the design of leading heat pipes for the space shuttle are reported. The analysis, de...
Titanium-water heat pipes are being investigated for use in heat rejection systems for lunar and Mar...
An evaluation is presented for the current heat pipe system on the OAO spacecraft, in order to incre...
Titanium-water heat pipes are being evaluated for use in the heat rejection system for space fission...
The construction of two test modules is presented for a feasibility demonstration of a concept for r...
The critical evaluation and subsequent redesign of the power conversion subsystem of the spacecraft ...
Heat pipe technology pertinent to the design and application of self-controlled, variable conductanc...
A gas-controlled variable-conductance heat pipe was qualified for flight aboard orbiting astronomica...
The activities presented in this paper focus on a new approach to provide passive regulation of the ...
The activities presented in this paper focus on a new approach to provide passive regulation of the ...
The feasibility of performance enhancing the sandwich panel heat pipe was investigated for moderate ...
This report covers the design, fabrication, and test of several dual slot heat pipe engineering deve...
The OAO-C spacecraft has three circular heat pipes, each of a different internal design, located in ...
Various heat pipe temperature control techniques are critically evaluated using characteristic featu...
As part of an effort to develop reliable, cost effective spacecraft thermal control heat pipes, life...
Development in the design of leading heat pipes for the space shuttle are reported. The analysis, de...
Titanium-water heat pipes are being investigated for use in heat rejection systems for lunar and Mar...
An evaluation is presented for the current heat pipe system on the OAO spacecraft, in order to incre...
Titanium-water heat pipes are being evaluated for use in the heat rejection system for space fission...
The construction of two test modules is presented for a feasibility demonstration of a concept for r...
The critical evaluation and subsequent redesign of the power conversion subsystem of the spacecraft ...
Heat pipe technology pertinent to the design and application of self-controlled, variable conductanc...
A gas-controlled variable-conductance heat pipe was qualified for flight aboard orbiting astronomica...
The activities presented in this paper focus on a new approach to provide passive regulation of the ...
The activities presented in this paper focus on a new approach to provide passive regulation of the ...
The feasibility of performance enhancing the sandwich panel heat pipe was investigated for moderate ...
This report covers the design, fabrication, and test of several dual slot heat pipe engineering deve...
The OAO-C spacecraft has three circular heat pipes, each of a different internal design, located in ...
Various heat pipe temperature control techniques are critically evaluated using characteristic featu...