A low-cost thermal control heat pipe having nearly covered grooves extruded in aluminum was developed at NASA. Analytical predictions of transport capability are in excellent agreement with experimental results using ammonia. Axial heat transport predictions as a function of fluid charge are presented also for methane, ethane, propane, and butane. Experimental tests show performance considerably better than that of open groove extruded pipes and comparing favorably with that of more complicated arterial/wick configurations. For ammonia at 20 C, the covert groove pipe obtained a static wicking height of 2.5 cm and an axial heat transport capability of 143 W-m
The objective of this program was to investigate analytically and experimentally the performance of ...
A gas-controlled variable-conductance heat pipe was qualified for flight aboard orbiting astronomica...
Heat pipes were developed which can be used as (1) a variable conductance link between a heat source...
As part of an effort to develop reliable, cost effective spacecraft thermal control heat pipes, life...
An experimental program to evaluate noncondensable gas generation in ammonia heat pipes was complete...
An evaluation is presented for the current heat pipe system on the OAO spacecraft, in order to incre...
An analysis was made of the cryogenic axial groove methane and axial groove nitrogen heat pipes. Dat...
Various heat pipe temperature control techniques are critically evaluated using characteristic featu...
Tests were performed on a high-capacity channel-wick heat pipe to assess the transport limitations o...
The OAO-C spacecraft has three circular heat pipes, each of a different internal design, located in ...
The development and use of heat pipes are described, including space requirements and contributions....
A technology evaluation study on axially grooved heat pipes is presented. The state-of-the-art is re...
An investigation to adapt axial grooved designs to the gammit of heat pipe thermal control technique...
Titanium-water heat pipes are being investigated for use in heat rejection systems for lunar and Mar...
Titanium-water heat pipes are being evaluated for use in the heat rejection system for space fission...
The objective of this program was to investigate analytically and experimentally the performance of ...
A gas-controlled variable-conductance heat pipe was qualified for flight aboard orbiting astronomica...
Heat pipes were developed which can be used as (1) a variable conductance link between a heat source...
As part of an effort to develop reliable, cost effective spacecraft thermal control heat pipes, life...
An experimental program to evaluate noncondensable gas generation in ammonia heat pipes was complete...
An evaluation is presented for the current heat pipe system on the OAO spacecraft, in order to incre...
An analysis was made of the cryogenic axial groove methane and axial groove nitrogen heat pipes. Dat...
Various heat pipe temperature control techniques are critically evaluated using characteristic featu...
Tests were performed on a high-capacity channel-wick heat pipe to assess the transport limitations o...
The OAO-C spacecraft has three circular heat pipes, each of a different internal design, located in ...
The development and use of heat pipes are described, including space requirements and contributions....
A technology evaluation study on axially grooved heat pipes is presented. The state-of-the-art is re...
An investigation to adapt axial grooved designs to the gammit of heat pipe thermal control technique...
Titanium-water heat pipes are being investigated for use in heat rejection systems for lunar and Mar...
Titanium-water heat pipes are being evaluated for use in the heat rejection system for space fission...
The objective of this program was to investigate analytically and experimentally the performance of ...
A gas-controlled variable-conductance heat pipe was qualified for flight aboard orbiting astronomica...
Heat pipes were developed which can be used as (1) a variable conductance link between a heat source...