Heat Transfer Thermal Control and Heat Pipes (Progress in astronautics and aeronautics) ePub download
- ISBN: 0915928396
- ISBN13: 978-0915928392
- ePub: 1531 kb | FB2: 1196 kb
- Language: English
- Category: Astronomy & Space Science
- Publisher: Amer Inst of Aeronautics & (June 1, 1980)
- Pages: 393
- Rating: 4.7/5
- Votes: 953
- Format: doc azw mbr lrf
In spacecraft design, the function of the thermal control system (TCS) is to keep all the spacecraft's component systems within acceptable temperature ranges during all mission phases
In spacecraft design, the function of the thermal control system (TCS) is to keep all the spacecraft's component systems within acceptable temperature ranges during all mission phases. It must cope with the external environment, which can vary in a wide range as the spacecraft is exposed to deep space or to solar or planetary flux, and with ejecting to space the internal heat generated by the operation of the spacecraft itself.
Start by marking Heat Transfer Thermal Control and Heat Pipes (Progress in astronautics and aeronautics) as. .
Start by marking Heat Transfer Thermal Control and Heat Pipes (Progress in astronautics and aeronautics) as Want to Read: Want to Read savin. ant to Read. Heat Transfer Thermal.
by Fluids, Plasma, and Heat Transfer Conference (3rd : 1982 : Saint Louis, M. Series: Progress in Astronautics and Aeronautics, V. 85.
Series: Progress in Astronautics and Aeronautics, V.
PDF Heat-balance thermal protection is non-ablating thermal protection for . Heat-pipe and high thermal conductivity material can both. control and heat-balance thermal protection. In early 1966, a first W-Li super high temperature heat-pipe was. developed.
PDF Heat-balance thermal protection is non-ablating thermal protection for leading edge of hypersonic vehicle. transfer heat isothermally. And embedded structure is more. In last century 70’s, heat-pipe was used for. heat control on space vehicles. heat-pipe as heat-balance thermal protection for missile. fin. Buffone used liquid metal (Na and Li) heat-pipe.
Progress in Astronautics and Aeronautics, Volume 20: Thermophysics of.
Progress in Astronautics and Aeronautics, Volume 20: Thermophysics of Spacecraft and Planetary Bodies: Radiation Properties of Solids and the Electromagnetic Radiation Environment in Space is a collection of technical papers drawn mainly from the American Institute of Aeronautics and Astronautics Thermophysics Specialist Conference, held in New Orleans on April 17-20, 1967. Part V contains papers on thermal similitude and on the closely related subject of radiant heat transfer analysis of thermal systems. Lastly, Part VI focuses on the heat transfer within the spacecraft under the conditions of space environment, specifically conductive and radiative transfer.
Heat Pipe Thermal Control View Factor Thermal Protection System Thermal Contact Conductance. Satellite Thermal Control for System Engineers, Progress in Aeronautics and Astronautics, Vol. 181, AIAA, Reston, 1998. These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves. 40. Meseguer, . Pérez-Grande, . and Sanz-Andrés, . Spacecraft Thermal Control, Woodhead Publishing, Oxford, 2011.
We will start by examining conduction heat transfer
We will start by examining conduction heat transfer. We must first determine how to relate the heat transfer to other properties (either mechanical, thermal, or geometrical). The answer to this is rooted in experiment, but it can be motivated by considering heat flow along a "bar" between two heat reservoirs at TA, TB as shown in Figure . To recap, there is an approximate relation between skin friction (momentum flux to the wall) and heat transfer called the Reynolds analogy that provides a useful way to estimate heat transfer rates in situations in which the skin friction is known. The relation is expressed by. St C f 2.
Keywords: heat pipes, performance characteristics, types of heat pipes, numerical modeling, heat pipe applications. This includes the steady and unsteady forced laminar and turbulent convective heat and mass transfer, compressible vapor effects, phase-change phenomena, boiling, tion, two-phase flow, rotating flows, thin film flows, liquid flow in porous media, rarefied gases, interfacial heat and mass transfer, flows, and conjugate heat transfer effects.
The paper presents an overview of heat pipes, especially those used in different space missions. Historical perspectives, principles of operations, types of heat pipes are discussed. Several factors have contributed to the science and technology of the present state-of-Art heat pipe leading to the development of loop heat pipes, micro and miniature heat pipes and micro loop heat pipes. The paper presents an overview of heat pipes, especially those used in different space missions.
The use of heat pipes as heat exchangers and heat transfer structural members allows creating a new generation of efficient heat removals on their basis. Today the following areas where heat pipes are widely used can be identified: computer equipment from small computers to large data centers, power electronics, and electronics for special purposes. The article analyzes the current state and prospects of using heat pipes in thermal control system of electronic equipment for ground applications. Keywords: heat pipe, thermosyphon, electronics, computer equipment, cooling system