A historical perspective on pumped-fluid loop space radiators provides a basis for the design of the Space Station Solar Dynamic (SD) power module radiator. SD power modules, capable of generating 25 kW (electrical) each, are planned for growth in Station power requirements. The Brayton cycle SD module configuration incorporates a pumped-fluid loop radiator that must reject up to 99 kW (thermal). The thermal/hydraulic design conditions in combination with required radiator orientation and packaging envelope form a unique set of constraints as compared to previous pumped-fluid loop radiator systems. Nevertheless, past program successes have demonstrated a technology base that can be applied to the SD radiator development program to ensure a ...
A government/industry team designed, built, and tested a 2 kWe solar dynamic space power system in a...
A government/industry team designed, built and tested a 2-kWe solar dynamic space power system in a ...
A study was performed to determine the potential performance and related technology requirements of ...
A two-part overview of progress in space radiator technologies is presented. The first part reviews ...
The Parabolic Offset Linearly Actuated Reflector (POLAR) solar dynamic module was selected as the ba...
Four advanced space radiator concepts that were pursued in an integrated effort to develop multi-mis...
Concept development work on space heat rejection subsystems tailored to the requirements of various ...
The Space Station Freedom Program is presently planned to consist of two phases. At the completion o...
A joint U.S./Russia program is being conducted to develop, fabricate, launch, and operate a solar dy...
A solar dynamic (SD) space power system has been under test at the NASA Lewis Research Center since ...
In April of 1997, the NASA Lewis Research Center hosted the testing of the photovoltaic thermal radi...
Mission planning documents were used to analyze the radiator design and thermal control surface requ...
An advanced radiator concept for heat rejection in space is described which uses a two-phase working...
An advanced heat pipe receiver designed for a solar dynamic space power system is described. The pow...
Major technical challenges which were met in the design and development of the Space Shuttle Orbiter...
A government/industry team designed, built, and tested a 2 kWe solar dynamic space power system in a...
A government/industry team designed, built and tested a 2-kWe solar dynamic space power system in a ...
A study was performed to determine the potential performance and related technology requirements of ...
A two-part overview of progress in space radiator technologies is presented. The first part reviews ...
The Parabolic Offset Linearly Actuated Reflector (POLAR) solar dynamic module was selected as the ba...
Four advanced space radiator concepts that were pursued in an integrated effort to develop multi-mis...
Concept development work on space heat rejection subsystems tailored to the requirements of various ...
The Space Station Freedom Program is presently planned to consist of two phases. At the completion o...
A joint U.S./Russia program is being conducted to develop, fabricate, launch, and operate a solar dy...
A solar dynamic (SD) space power system has been under test at the NASA Lewis Research Center since ...
In April of 1997, the NASA Lewis Research Center hosted the testing of the photovoltaic thermal radi...
Mission planning documents were used to analyze the radiator design and thermal control surface requ...
An advanced radiator concept for heat rejection in space is described which uses a two-phase working...
An advanced heat pipe receiver designed for a solar dynamic space power system is described. The pow...
Major technical challenges which were met in the design and development of the Space Shuttle Orbiter...
A government/industry team designed, built, and tested a 2 kWe solar dynamic space power system in a...
A government/industry team designed, built and tested a 2-kWe solar dynamic space power system in a ...
A study was performed to determine the potential performance and related technology requirements of ...