The development of a Dewar system for handling liquid helium under weightless conditions is described. Porous plug designs for the prevention of superfluid creep out of the dewar through the vent line were evaluated. For the purpose of designing a neck to provide a transition from the cold cavity to the outside, the loads carried by the neck and equipment supports were studied. Temperature, pressure, and mass flow instrumentation for monitoring Dewar performance were also evaluated. In addition, multilayer blankets consisting of aluminized Mylar separated by Dacron net sheets were designed to insulate the pressure vessel. The dewar system is suggested for use with the star tracking telescope aboard the relativity satellite
Long-term active operation of Dewar vessels for liquid helium is connected with the risk of their da...
Recent advances in the technology of infrared detectors have made possible a wide range of scientifi...
In the development of flight insulation systems for large cryogenic orbital storage (spray on foam a...
Astrophysical observations at millimeter wavelengths require large (2-to-5- meter diameter) telescop...
A feasible concept for a launchable three year lifetime helium dewar was investigted. Current helium...
A number of space flight experiments and entire facilities require superfluid helium as a coolant. A...
Thermal performance evaluations (TPE) were conducted with the superfluid helium dewar of the Infrare...
The aircraft-based Stratospheric Observatory for Infrared Astronomy (SOFIA) is a platform for multip...
Pressure rise characteristics of liquid hydrogen dewar for homogeneous, normal-gravity quiescent, an...
The ASTROMAG facility is the heart of a large charged particle detection and resolution system. ASTR...
The Instrument Test Dewar (ITD) is a cryogenic facility designed and built to test Cosmic Background...
The results are presented of a study program directed toward evaluating the problems associated with...
The Soft Xray Spectrometer (SXS) instrument on-board the ASTRO-H X-ray mission is based on microcalo...
Long-term active operation of Dewar vessels for liquid helium is connected with the risk of their da...
Storag of helium gas at higher temperature and pressure using liquid hydrogen refrigerant to surroun...
Long-term active operation of Dewar vessels for liquid helium is connected with the risk of their da...
Recent advances in the technology of infrared detectors have made possible a wide range of scientifi...
In the development of flight insulation systems for large cryogenic orbital storage (spray on foam a...
Astrophysical observations at millimeter wavelengths require large (2-to-5- meter diameter) telescop...
A feasible concept for a launchable three year lifetime helium dewar was investigted. Current helium...
A number of space flight experiments and entire facilities require superfluid helium as a coolant. A...
Thermal performance evaluations (TPE) were conducted with the superfluid helium dewar of the Infrare...
The aircraft-based Stratospheric Observatory for Infrared Astronomy (SOFIA) is a platform for multip...
Pressure rise characteristics of liquid hydrogen dewar for homogeneous, normal-gravity quiescent, an...
The ASTROMAG facility is the heart of a large charged particle detection and resolution system. ASTR...
The Instrument Test Dewar (ITD) is a cryogenic facility designed and built to test Cosmic Background...
The results are presented of a study program directed toward evaluating the problems associated with...
The Soft Xray Spectrometer (SXS) instrument on-board the ASTRO-H X-ray mission is based on microcalo...
Long-term active operation of Dewar vessels for liquid helium is connected with the risk of their da...
Storag of helium gas at higher temperature and pressure using liquid hydrogen refrigerant to surroun...
Long-term active operation of Dewar vessels for liquid helium is connected with the risk of their da...
Recent advances in the technology of infrared detectors have made possible a wide range of scientifi...
In the development of flight insulation systems for large cryogenic orbital storage (spray on foam a...