This paper focuses on the flight results of the Cryogenic Two-Phase Flight Experiment (CRYOTP), which was a Hitchhiker based experiment that flew on the space shuttle Columbia in March of 1994 (STS-62). CRYOTP tested two new technologies for advanced cryogenic thermal control; the Space Heat Pipe (SHP), which was a constant conductance cryogenic heat pipe, and the Brilliant Eyes Thermal Storage Unit (BETSU), which was a cryogenic phase-change thermal storage device. These two devices were tested independently during the mission. Analysis of the flight data indicated that the SHP was unable to start in either of two attempts, for reasons related to the fluid charge, parasitic heat leaks, and cryocooler capacity. The BETSU test article was su...
Design of the two-phase systems which are anticipated to be utilized in future spacecraft thermal ma...
System studies required to verify a tube-in-tube cryogenic heat exchanger as optimum for the space s...
An analysis was made of the cryogenic axial groove methane and axial groove nitrogen heat pipes. Dat...
This paper presents an overview of the Cryogenic Test Bed (CTB) experiments including experiment res...
This paper describes the engineering thought process behind the failure analysis, redesign, and rewo...
In May 1996, the Brilliant Eyes Ten-Kelvin Sorption Cryocooler Experiment (BETSCE) was flown aboard ...
Cryogenic loop heat pipe (CLHP) is one of the key components in the future space infrared exploratio...
The Thermal Energy Storage Flight Experiment was designed to characterize void shape and location in...
In the development of flight insulation systems for large cryogenic orbital storage (spray on foam a...
This paper details the flight configuration and pre-flight performance test results of the fifth gen...
The Center for Space Engineering at Utah State University and NASA’s Jet Propulsion Laboratory have ...
The Wide Field Infrared Explorer was developed to perform astronomy using a cryogenically cooled inf...
This paper reviews the history of cryogenic fluid management technology development and infusion int...
Launch operations engineers at the Kennedy Space Center have identified an Integrated Refrigeration ...
A flat-plate heat pipe (FPHP) experiment has been set up for micro-gravity tests on a NASA supplied ...
Design of the two-phase systems which are anticipated to be utilized in future spacecraft thermal ma...
System studies required to verify a tube-in-tube cryogenic heat exchanger as optimum for the space s...
An analysis was made of the cryogenic axial groove methane and axial groove nitrogen heat pipes. Dat...
This paper presents an overview of the Cryogenic Test Bed (CTB) experiments including experiment res...
This paper describes the engineering thought process behind the failure analysis, redesign, and rewo...
In May 1996, the Brilliant Eyes Ten-Kelvin Sorption Cryocooler Experiment (BETSCE) was flown aboard ...
Cryogenic loop heat pipe (CLHP) is one of the key components in the future space infrared exploratio...
The Thermal Energy Storage Flight Experiment was designed to characterize void shape and location in...
In the development of flight insulation systems for large cryogenic orbital storage (spray on foam a...
This paper details the flight configuration and pre-flight performance test results of the fifth gen...
The Center for Space Engineering at Utah State University and NASA’s Jet Propulsion Laboratory have ...
The Wide Field Infrared Explorer was developed to perform astronomy using a cryogenically cooled inf...
This paper reviews the history of cryogenic fluid management technology development and infusion int...
Launch operations engineers at the Kennedy Space Center have identified an Integrated Refrigeration ...
A flat-plate heat pipe (FPHP) experiment has been set up for micro-gravity tests on a NASA supplied ...
Design of the two-phase systems which are anticipated to be utilized in future spacecraft thermal ma...
System studies required to verify a tube-in-tube cryogenic heat exchanger as optimum for the space s...
An analysis was made of the cryogenic axial groove methane and axial groove nitrogen heat pipes. Dat...