The behavior of materials in the space environment continues to be a limiting technology for spacecraft and experiments. The thermal control surfaces experiment (TCSE) aboard the Long Duration Exposure Facility (LDEF) is the most comprehensive experiment flown to study the effects of the space environment on thermal control surfaces. Selected thermal control surfaces were exposed to the LDEF orbital environment and the effects of this exposure were measured. The TCSE combined in-space orbital measurements with pre and post-flight analyses of flight materials to determine the effects of long term space exposure. The TCSE experiment objective, method, and measurements are described along with the results of the initial materials analysis. The...
Water cascade heat pump system design and developed for continuous operation in thermal control syst...
A spacecraft presents a unique design challenge with respect to providing a comfortable environment ...
The capabilities of the atmospheric modeling and sensor simulation (AMASS) system were studied in or...
The capability of the orbiter environmental control and life support system (ECLSS) to support vehic...
The Space Shuttle Orbiter Thermal Protection System materials, design approaches associated with eac...
The Thermal Control Surfaces Experiment (TCSE) is the most complex system, other than the LDEF, retr...
The issue of the effects of the space environment on spacecraft needs to be understood for the long ...
A core facility capable of performing a majority of materials processing experiments is discussed. E...
The long term effects of the natural and induced space environment on spacecraft surfaces are critic...
Tests were conducted to determine the effects of electrostatic propulsion beam divergence effects on...
The experimental program which was conducted in the Calspan 96-inch hypersonic shock tunnel to inves...
The Marshall Space Flight Center conducts research programs in space sciences, materials processing ...
The study of long term near ultra-violet (NUV) effects in a vacuum atmosphere, is a crucial element ...
The 'development of sensors for ceramic components in advanced propulsion systems' program is divide...
Calibration method and ultrahigh vacuum components for ionization gage and mass spectromete
Water cascade heat pump system design and developed for continuous operation in thermal control syst...
A spacecraft presents a unique design challenge with respect to providing a comfortable environment ...
The capabilities of the atmospheric modeling and sensor simulation (AMASS) system were studied in or...
The capability of the orbiter environmental control and life support system (ECLSS) to support vehic...
The Space Shuttle Orbiter Thermal Protection System materials, design approaches associated with eac...
The Thermal Control Surfaces Experiment (TCSE) is the most complex system, other than the LDEF, retr...
The issue of the effects of the space environment on spacecraft needs to be understood for the long ...
A core facility capable of performing a majority of materials processing experiments is discussed. E...
The long term effects of the natural and induced space environment on spacecraft surfaces are critic...
Tests were conducted to determine the effects of electrostatic propulsion beam divergence effects on...
The experimental program which was conducted in the Calspan 96-inch hypersonic shock tunnel to inves...
The Marshall Space Flight Center conducts research programs in space sciences, materials processing ...
The study of long term near ultra-violet (NUV) effects in a vacuum atmosphere, is a crucial element ...
The 'development of sensors for ceramic components in advanced propulsion systems' program is divide...
Calibration method and ultrahigh vacuum components for ionization gage and mass spectromete
Water cascade heat pump system design and developed for continuous operation in thermal control syst...
A spacecraft presents a unique design challenge with respect to providing a comfortable environment ...
The capabilities of the atmospheric modeling and sensor simulation (AMASS) system were studied in or...