The objective was to measure liquid mass to plus or minus 1 percent in two-phase tanks in orbit. Viewgraphs present information on concept selection, program status and anticipated results. The program aims at test results showing 1 percent accuracy, the development of a breadboard test article usable in the lab or aboard a KC-135, and a concept that will permit flight article design to proceed
Two-dimensional shell models of the portion of the solid rocket booster (SRB) with the external tank...
Theoretical and experimental studies of graphite and unspecified reactor material oxidation behavior...
Surveyor project progress in flight and ground testing, mission operations and planning, vehicle dev...
The purpose was to identify recent thermal analysis efforts and to review that part of the analysis ...
The results of a technical audit of the Space Station Freedom Program conducted by the Program Direc...
Potential scientific uses of the external tanks were examined. An onorbit conversion of the external...
Adaptability of Lunar Orbiter to surface experiments using flyby and earth return trajector
The use of Heavy Lift Launch Vehicles (HLLVs) for Space Station assembly, logistics. and resupply is...
Working group goals for this year are: Goal 1. Due to many review comments the green books will be u...
Definition of design/operations requirements for support of human productivity, identification of pr...
This presentation focuses on COTS Battery testing for energy content, toxicity, hazards, failures mo...
Primary avionics software system; software development approach; user support and problem diagnosis;...
A laboratory experiment was conducted to quantify the annoyance of people to the flyover noise of ad...
The three-dimensional finite element modeling techniques developed for the thermal analysis of a hyp...
The results of a NASA in-house team effort to develop a concept definition for a Commercially Develo...
Two-dimensional shell models of the portion of the solid rocket booster (SRB) with the external tank...
Theoretical and experimental studies of graphite and unspecified reactor material oxidation behavior...
Surveyor project progress in flight and ground testing, mission operations and planning, vehicle dev...
The purpose was to identify recent thermal analysis efforts and to review that part of the analysis ...
The results of a technical audit of the Space Station Freedom Program conducted by the Program Direc...
Potential scientific uses of the external tanks were examined. An onorbit conversion of the external...
Adaptability of Lunar Orbiter to surface experiments using flyby and earth return trajector
The use of Heavy Lift Launch Vehicles (HLLVs) for Space Station assembly, logistics. and resupply is...
Working group goals for this year are: Goal 1. Due to many review comments the green books will be u...
Definition of design/operations requirements for support of human productivity, identification of pr...
This presentation focuses on COTS Battery testing for energy content, toxicity, hazards, failures mo...
Primary avionics software system; software development approach; user support and problem diagnosis;...
A laboratory experiment was conducted to quantify the annoyance of people to the flyover noise of ad...
The three-dimensional finite element modeling techniques developed for the thermal analysis of a hyp...
The results of a NASA in-house team effort to develop a concept definition for a Commercially Develo...
Two-dimensional shell models of the portion of the solid rocket booster (SRB) with the external tank...
Theoretical and experimental studies of graphite and unspecified reactor material oxidation behavior...
Surveyor project progress in flight and ground testing, mission operations and planning, vehicle dev...