INES - PDFSEARCH.IO - Document Search Engine

INES
Results: 938

#	Item
131	EXTRACTION OF LOW DISPERSION SPECTRA FOR INES P.M. Rodr´ıguez-Pascual1 , N. Schartel2,3 , erez-Calpena4 W. Wamsteker2,3 , A. P´ 1 Add to Reading List Source URL: ines.ts.astro.it Language: English - Date: 2001-02-23 07:05:16
132	Chapter 11 Calibration of the Net Flux 11.1 Low-Dispersion Absolute Flux Calibration Add to Reading List Source URL: ines.oat.ts.astro.it Language: English - Date: 2001-02-23 07:05:18
133	Chapter 9 Low-Dispersion Flux Extraction (SWET ) Spectral data are extracted from the two-dimensional (2-D) low-dispersion resampled images (SI) using a signal weighted extraction technique (SWET ). This technique provid Add to Reading List Source URL: ines.ts.astro.it Language: English - Date: 2001-02-23 07:05:18
134	Power Subsystem. The power subsystem on the IUE spacecraft is a direct energy transfer (DET) system. The primary source of power is the spacecraft solar array which consists of two deployable paddles mounted to Add to Reading List Source URL: ines.ts.astro.it Language: English - Date: 2001-02-23 07:05:19
135	The Onboard Computer. The onboard computer (OBC) maintains attitude control and controls the scientific experiment operation. Because it is so vital to spacecraft operation, the OBC must be highly reliable. The Add to Reading List Source URL: ines.ts.astro.it Language: English - Date: 2001-02-23 07:05:20
136	Operations highlight summaryJanuary 26. The International Ultraviolet Explorer was launched, at 17:36 UT, with an initial plan of revolving Add to Reading List Source URL: ines.oat.ts.astro.it Language: English - Date: 2001-02-23 07:05:19
137	CONCATENATION AND REBINNING OF IUE HIGH RESOLUTION SPECTRA Enrique Solano1 1 INSA. ESA-IUE Observatory. P.O. BoxMadrid (Spain). Add to Reading List Source URL: ines.oat.ts.astro.it Language: English - Date: 2001-02-23 07:05:20
138	Chapter 12 Final Archive Data Products The output files for the IUE Final Archive are fundamentally different from those produced by IUESIPS, both in content and format. They are based on the Flexible Image Transport Sys Add to Reading List Source URL: ines.ts.astro.it Language: English - Date: 2001-02-23 07:05:18
139	Spacecraft Thermal Design. The purpose of the thermal control design is to maintain all of the elements of the spacecraft system within their temperature limits for all mission phases. From this viewpoint, the IU Add to Reading List Source URL: ines.ts.astro.it Language: English - Date: 2001-02-23 07:05:20
140	Chapter 14 Core Data Items To fully and accurately characterize the IUE dataset and facilitate future analysis, a group of “core data items” descriptive of each image was identified. These core data items (CDIs) are Add to Reading List Source URL: ines.oat.ts.astro.it Language: English