Ad
related to: thermal control system in spacecraft
Search results
Results From The WOW.Com Content Network
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 the extreme coldness found in the shadows of deep ...
ISS External Active Thermal Control System (EATCS) diagram Early Ammonia Servicer DDCU cold plate design. The International Space Station (ISS) External Active Thermal Control System (EATCS) [1] maintains an equilibrium when the ISS environment or heat loads exceed the capabilities of the Passive Thermal Control System (PTCS).
Space Shuttle Discovery as it approaches the International Space Station during the STS-114 on 28 July 2005. The Space Shuttle thermal protection system (TPS) is the barrier that protected the Space Shuttle Orbiter during the extreme 1,650 °C (3,000 °F) heat of atmospheric reentry. A secondary goal was to protect from the heat and cold of ...
EECOM's revamped Space Shuttle responsibilities included the atmospheric pressure control and revitalization systems, the cooling systems (air, water, and freon), and the supply/waste water system. EECOM's critical function was to maintain the systems, such as atmosphere and thermal control, that keep the crew alive.
Satellite Thermal Control Handbook, ed. David Gilmore. ISBN 1-884989-00-4. In particular, Chapter 5, Insulation, by Martin Donabedian and David Gilmore. Tutorial on temperature control of spacecraft by JPL "Cassini dons its thermal cloak" (Press release). NASA JPL. 1997-01-03. Archived from the original on 2007-09-04
Control theory for the design of the attitude and orbit control subsystem, which points the spacecraft correctly, and maintains or changes the orbit according to the mission profile; the hardware used for actuation and sensing in space is usually very specific to spacecraft, Thermal engineering for the design of the thermal control subsystem ...
Such space systems require advanced high-temperature thermal control systems. Liquid metal heat pipes with conventional radiators are considered ideally suited for such applications. [5] However, the required radiator surface area is huge, hence, the system mass is very large. The liquid droplet radiator (LDR) has an advantage in terms of the ...
Swales & Associates, Inc., doing business as Swales Aerospace, was an aerospace engineering firm based in Maryland. It was employee-owned through an ESOP.Swales did some manufacturing of aerospace-related products, specializing in structural and thermal management systems—ways to control movement and heat in satellites.