Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Denis R. Mahony"'
Publikováno v:
15th International Energy Conversion Engineering Conference.
Publikováno v:
Proceeding of Second Thermal and Fluids Engineering Conference.
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
The ability to accurately calculate the rate of fluid flow in a Loop Heat Pipe (LHP) is essential in the analytical modeling of the loop performance. The first step in the process of validating a LHP model is, therefore, to verify the predicted flow
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Loop Heat Pipes (LHPs) have proven themselves as reliable and robust heat transport devices for spacecraft thermal control systems (TCS). As they gained increasing acceptance, LHP-based TCS have become more and more complex; more than one LHP may be
Autor:
Bang N. Nguyen, William C. Robinson, Denis R. Mahony, Triem T. Hoang, William J. Armiger, Robert W. Baldauff, Alexandria Va
Publikováno v:
42nd International Conference on Environmental Systems.
The Central Thermal Bus design of the TacSat 4 spacecraft thermal control system (TCS) utilized an ammonia Loop Heat Pipe (LHP) to acquire/transport waste heat from the onboard electronics and reject it to space via eight radiator panels. The TCS und
Publikováno v:
42nd AIAA Thermophysics Conference.
Loop Heat Pipes (LHPs) have become the mainstay of the spacecraft thermal control systems (TCS) over the last 10 years. Usage of LHPs enables the TCS to carry out many thermal management functions that could not be performed in the past, particularly
Publikováno v:
9th Annual International Energy Conversion Engineering Conference.
Loop Heat Pipes (LHPs) have replaced the conventional heat pipes as the primary heat transports for the spacecraft thermal control systems (TCS). For the most part, the LHP operational capability and versatility provide the engineers many design opti
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Variable Conductance Heat Pipes (VCHPs) have been used in spacecraft thermal control systems (TCS) for more than 25 years. Being heat-driven capillary-pumped heat transport devices, they are extremely reliable, durable and, more importantly, maintena
Autor:
Phillip P. Jenkins, Robert J. Walters, Michael J. Krasowski, John J. Chapman, Perry G. Ballard, John A. Vasquez, Denis R. Mahony, Susie N. LaCava, William R. Braun, Robert Skalitzky, Norman F. Prokop, Joseph M. Flatico, Lawrence C. Greer, Karen B. Gibson, William H. Kinard, H. Gary Pippin, Jacob I. Kleiman
Publikováno v:
AIP Conference Proceedings.
The Materials on the International Space Station Experiments (MISSE) provide low‐cost material exposure experiments on the exterior of the International Space Station (ISS). The original concept for a suitcase‐like box bolted to the ISS to passiv
Publikováno v:
SAE Technical Paper Series.