Electrochromic Variable Emittance Devices on Silicon Wafer for Spacecraft Thermal Control

Statistics – Applications

Scientific paper

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

Spaceborne And Space Research Instruments, Apparatus, And Components, Thermal Instruments And Apparatus

Scientific paper

Small light-weight satellites and space vehicles under development for future NASA missions have reduced thermal mass and are strongly affected by changes in orbital conditions, resulting in large temperature variations. Restrictions on payload weight and volume limit the usefulness of many thermal control technologies. One thermal control approach, being considered by NASA in both nano- and micro- spacecraft applications, involves the use of electrochromic (EC) variable emittance devices (VEDs). VEDs operating in the harsh space environment (UV radiation, atomic oxygen) must be properly protected if they are to reach their design operational life. In this paper, we discuss the design of an all-solid-state EC VED built on a silicon wafer. The silicon wafer serves as a window for IR radiation and protects EC layers from the space environment. This paper also discusses the expected limits of emittance modulation of the EC VED on the silicon substrate as well as possible impact of an antireflective coating on IR emittance modulation.

No associations

LandOfFree

Say what you really think

Search LandOfFree.com for scientists and scientific papers. Rate them and share your experience with other people.

Rating

Electrochromic Variable Emittance Devices on Silicon Wafer for Spacecraft Thermal Control does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Electrochromic Variable Emittance Devices on Silicon Wafer for Spacecraft Thermal Control, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Electrochromic Variable Emittance Devices on Silicon Wafer for Spacecraft Thermal Control will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFWR-SCP-O-1601241

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.