DocumentCode
1747134
Title
STRV-1d QWIP technology validation in space flight
Author
Kenny, James T. ; Pollock, Harold R.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
1
fYear
2001
fDate
2001
Abstract
New technologies are arriving on the scene that promise enhancement or new capabilities. Some of these technologies have potential for NASA and DOD space-based applications. In these cases, the technology must be demonstrated and validated to a degree that risk may be balanced for the space mission roles. Quantum Well Infrared Photodetector (QWIP) is one of these technologies. QWIP has a variety of space-based applications in the 8 to 16 μm wavelength range. Radiation tolerance and higher operating temperature are potentially significant benefits for long duration missions. In this paper, we describe the selection of and preparation for a mission that provides the opportunity to demonstrate and validate QWIP FPA in the natural, space radiation environment. We discuss the objectives of this demonstration opportunity, and the development and test steps required to deliver the QWIP Experiment to space
Keywords
infrared detectors; quantum well devices; radiation hardening (electronics); space vehicle electronics; 8 to 16 micrometre; QWIP technology validation; STRV-1d; long duration missions; operating temperature; quantum well infrared photodetector; radiation tolerance; space flight; space-based applications; test steps; Current measurement; Dark current; Extraterrestrial measurements; Infrared detectors; NASA; Propulsion; Sensor arrays; Space technology; Stability; Temperature;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2001, IEEE Proceedings.
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-6599-2
Type
conf
DOI
10.1109/AERO.2001.931708
Filename
931708
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