The thermomechanical fatigue (TMF) behavior of three continuous-fiber ceramic composites (CFCC's) was examined. The three matrices consisted of two different glass-ceramics and silicon carbide, respectively. The matrices of some of the specimens with the silicon carbide matrix were enhanced to improve oxidation resistance. All three were reinforced with Nicalon fibers with various fiber architectures. The thermoelastic properties of the matrix relative to the fibers, the elastic moduli and coefficients of thermal expansion (CTE), were different in each composite, providing a comparison of the effects of these critical properties. The specimens were tested under in-phase (IP) and out-of-phase (OP) cyclic loadings with respect to thermal cycl...
During the period April 29 through May 2, 1985, the Atmospheric Trace Molecule Spectroscopy (ATMOS) ...
Viewgraphs are presented which outline the overall system and component concepts for a 60 GHz inters...
The objective of this study is to model the on-orbit vibration environment encountered by a SmallSat...
A study was conducted under MSFC contract NAS8-39210 to compare tripropellant and bipropellant engin...
Performance characteristics of auxiliary inlet ejector nozzle configurations for takeoff, transonic ...
Viewgraphs on controlled structures technology presented at the steering committee workshop on 22-23...
The model nozzle configurations, acoustic test conditions, and detailed test results from the hot st...
Role of chemical reactions in comminution mechanism of ductile metals into ultrafine powders by grin...
Seventy-four pilots were monitored before, during, and after 3- or 4-day commercial short-haul trip ...
This report consists of data computed at the U.S. Space Command, GSFC, or provided by satellite owne...
This document is the Executive Summary of a technical report on a probabilistic risk assessment (PRA...
This report highlights key projects and technologies at Johnson Space Center for 1997. The report fo...
A regeneratively cooled thrust chamber has been designed and fabricated, consisting of an inner TD n...
An investigation to determine the rate of descent, the horizontal velocity, and the attitude at cont...
This model was trained by kan-bayashi using ruslan/tts1 recipe in espnet. Python API See htt...
During the period April 29 through May 2, 1985, the Atmospheric Trace Molecule Spectroscopy (ATMOS) ...
Viewgraphs are presented which outline the overall system and component concepts for a 60 GHz inters...
The objective of this study is to model the on-orbit vibration environment encountered by a SmallSat...
A study was conducted under MSFC contract NAS8-39210 to compare tripropellant and bipropellant engin...
Performance characteristics of auxiliary inlet ejector nozzle configurations for takeoff, transonic ...
Viewgraphs on controlled structures technology presented at the steering committee workshop on 22-23...
The model nozzle configurations, acoustic test conditions, and detailed test results from the hot st...
Role of chemical reactions in comminution mechanism of ductile metals into ultrafine powders by grin...
Seventy-four pilots were monitored before, during, and after 3- or 4-day commercial short-haul trip ...
This report consists of data computed at the U.S. Space Command, GSFC, or provided by satellite owne...
This document is the Executive Summary of a technical report on a probabilistic risk assessment (PRA...
This report highlights key projects and technologies at Johnson Space Center for 1997. The report fo...
A regeneratively cooled thrust chamber has been designed and fabricated, consisting of an inner TD n...
An investigation to determine the rate of descent, the horizontal velocity, and the attitude at cont...
This model was trained by kan-bayashi using ruslan/tts1 recipe in espnet. Python API See htt...
During the period April 29 through May 2, 1985, the Atmospheric Trace Molecule Spectroscopy (ATMOS) ...
Viewgraphs are presented which outline the overall system and component concepts for a 60 GHz inters...
The objective of this study is to model the on-orbit vibration environment encountered by a SmallSat...