Add to ORKGConsiderations associated with design of thermal subsystem of Orbiting Astronomical Observator
This work is the result of an 8-month cooperation between the author and IDS S.p.A. Company, which i...
A high temperature reusable surface insulation (HRSI) tile taken from the Space Shuttle orbiter was ...
Computer program for computation of thermal radiation heat loads and temperatures of spacecraft orbi...
Program computes the thermal environment of a spacecraft in a lunar orbit. The quantities determined...
The purpose of this report was to analyze the heat-transfer problem posed by the determination of sp...
The advantages and possible pitfalls of using a generalized method of measuring and, based on these ...
This paper describes a complete methodology for the computation of transient external heat fluxes (i...
Temperature gradients for analyzing surface distortions of magnesium solar collector in ecliptic ear...
External and internal passive and active methods for spacecraft thermal control - material insulatio...
In spacecraft missions it is vital to maintain all spacecraft components within their required tempe...
Graphical representation of orbital heat balance in form of polar diagrams is obtained from integral...
In spacecraft missions it is vital to maintain all spacecraft components within their required tempe...
In spacecraft missions it is vital to maintain all spacecraft components within their required tempe...
In spacecraft missions it is vital to maintain all spacecraft components within their required tempe...
Considerations associated with design of thermal subsystem of Orbiting Astronomical Observator
This work is the result of an 8-month cooperation between the author and IDS S.p.A. Company, which i...
A high temperature reusable surface insulation (HRSI) tile taken from the Space Shuttle orbiter was ...
Computer program for computation of thermal radiation heat loads and temperatures of spacecraft orbi...
Program computes the thermal environment of a spacecraft in a lunar orbit. The quantities determined...
The purpose of this report was to analyze the heat-transfer problem posed by the determination of sp...
The advantages and possible pitfalls of using a generalized method of measuring and, based on these ...
This paper describes a complete methodology for the computation of transient external heat fluxes (i...
Temperature gradients for analyzing surface distortions of magnesium solar collector in ecliptic ear...
External and internal passive and active methods for spacecraft thermal control - material insulatio...
In spacecraft missions it is vital to maintain all spacecraft components within their required tempe...
Graphical representation of orbital heat balance in form of polar diagrams is obtained from integral...
In spacecraft missions it is vital to maintain all spacecraft components within their required tempe...
In spacecraft missions it is vital to maintain all spacecraft components within their required tempe...
In spacecraft missions it is vital to maintain all spacecraft components within their required tempe...
Considerations associated with design of thermal subsystem of Orbiting Astronomical Observator
This work is the result of an 8-month cooperation between the author and IDS S.p.A. Company, which i...
A high temperature reusable surface insulation (HRSI) tile taken from the Space Shuttle orbiter was ...