The purpose was to identify recent thermal analysis efforts and to review that part of the analysis that addresses the prediction of fluid and container temperature gradients during low gravity storage in space. It was concluded that both small and large tanks require hundreds of hours to reach even 60 PSIA. In about 1000 hours, the small tank is close to equilibrium; the large tank requires many thousands of hours to reach equilibrium
This presentation focuses on COTS Battery testing for energy content, toxicity, hazards, failures mo...
The continuing examination of widely varied space shuttle concepts makes an understanding of concept...
The Human Occupied Space Teleoperator (HOST) system currently under development utilizes a flexible ...
The objective was to measure liquid mass to plus or minus 1 percent in two-phase tanks in orbit. Vie...
Adaptability of Lunar Orbiter to surface experiments using flyby and earth return trajector
Two-dimensional shell models of the portion of the solid rocket booster (SRB) with the external tank...
The results of a technical audit of the Space Station Freedom Program conducted by the Program Direc...
The results of a NASA in-house team effort to develop a concept definition for a Commercially Develo...
Definition of design/operations requirements for support of human productivity, identification of pr...
The use of Heavy Lift Launch Vehicles (HLLVs) for Space Station assembly, logistics. and resupply is...
Primary avionics software system; software development approach; user support and problem diagnosis;...
Potential scientific uses of the external tanks were examined. An onorbit conversion of the external...
Changes in coating morphology of mullite, silica, and ceramic mullite fiber at two heating rates are...
Working group goals for this year are: Goal 1. Due to many review comments the green books will be u...
The refrigeration cycles investigated are referred to as Joule-Thomson cycles because they depend on...
This presentation focuses on COTS Battery testing for energy content, toxicity, hazards, failures mo...
The continuing examination of widely varied space shuttle concepts makes an understanding of concept...
The Human Occupied Space Teleoperator (HOST) system currently under development utilizes a flexible ...
The objective was to measure liquid mass to plus or minus 1 percent in two-phase tanks in orbit. Vie...
Adaptability of Lunar Orbiter to surface experiments using flyby and earth return trajector
Two-dimensional shell models of the portion of the solid rocket booster (SRB) with the external tank...
The results of a technical audit of the Space Station Freedom Program conducted by the Program Direc...
The results of a NASA in-house team effort to develop a concept definition for a Commercially Develo...
Definition of design/operations requirements for support of human productivity, identification of pr...
The use of Heavy Lift Launch Vehicles (HLLVs) for Space Station assembly, logistics. and resupply is...
Primary avionics software system; software development approach; user support and problem diagnosis;...
Potential scientific uses of the external tanks were examined. An onorbit conversion of the external...
Changes in coating morphology of mullite, silica, and ceramic mullite fiber at two heating rates are...
Working group goals for this year are: Goal 1. Due to many review comments the green books will be u...
The refrigeration cycles investigated are referred to as Joule-Thomson cycles because they depend on...
This presentation focuses on COTS Battery testing for energy content, toxicity, hazards, failures mo...
The continuing examination of widely varied space shuttle concepts makes an understanding of concept...
The Human Occupied Space Teleoperator (HOST) system currently under development utilizes a flexible ...