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Cryogenic thermal distortion model validation for the jwst isim structure
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cofie, Emmanuel Johnston, John |
| Copyright Year | 2011 |
| Description | The James Webb Space Telescope (JWST) is a large, infrared-optimized space telescope consisting of an Optical telescope element (OTE), Integrated science instrument module (ISIM), a Spacecraft, and a Sunshield. The Integrated Science Instrument Module (ISIM) consists of the JWST science instruments (NIRCam, MIRI, NIRSpec), a fine guidance sensor (FGS), the ISIM Structure, and thermal and electrical subsystems. JWST's instruments are designed to work primarily in the infrared range of the electromagnetic spectrum, and the instruments and telescope operate at cryogenic temperatures (approximately 35 K for the instruments). |
| File Size | 1334319 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20110022515 |
| Archival Resource Key | ark:/13960/t4sj6g87k |
| Language | English |
| Publisher Date | 2011-08-25 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Low Temperature Tests Finite Element Method James Webb Space Telescope Spacecraft Instruments Surface Distortion Infrared Telescopes Space Temperature Cryogenics Mathematical Models Thermal Buckling Spacecraft Structures Cryogenic Temperature Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
