Title :
The Space Technology 8 mission
Author :
Franklin, Stan ; Jentung Ku ; Spence, Brian ; McEachen, M. ; White, Steve ; Samson, Jonathan ; Some, Rafael ; Zsoldos, Jennifer
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
Abstract :
The Space Technology 8 (ST8) mission is the latest in NASA´s New Millennium Program technology demonstration missions. ST8 includes a spacecraft bus built by industry, flying four new technology payloads in low-Earth orbit. This paper describes each payload, along with a brief description of the mission and spacecraft. The payloads include a miniature loop heat pipe intended to save mass and power on future small satellites, designed and built by NASA´s Goddard Space Flight Center; a lightweight, 35g/m linear mass, 40-m deployable boom intended as a future solar sail mast built by ATK Space Systems; a deployable, lightweight ultraflex solar array producing 175W/kg, also built by ATK Space Systems; and a high-speed, parallel-processing computer system built of state-of-the-art COTS processors, demonstrating SEU tolerance without the need for radiation-hardened electronics, and 100M operations per second per Watt processing throughput density
Keywords :
fault tolerant computing; heat pipes; parallel processing; solar cell arrays; space vehicles; technology; 40 m; New Millennium Program; SEU tolerance; Space Technology 8 mission; low-Earth orbit; miniature loop heat pipe; parallel-processing computer system; small satellites; solar sail mast; spacecraft bus; state-of-the-art COTS processors; technology demonstration missions; technology payloads; ultraflex solar array; Aerospace industry; Concurrent computing; Optical arrays; Payloads; Satellites; Solar heating; Space heating; Space technology; Space vehicles; Throughput;
Conference_Titel :
Aerospace Conference, 2006 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-9545-X
DOI :
10.1109/AERO.2006.1655767