DocumentCode :
3054077
Title :
Testing tether dynamics in space - the STRING mission
Author :
Altan, B. ; Forquera, P. ; Segal, Y.
Author_Institution :
Dept. of Aeronaut. & Astronaut., Stanford Univ., CA, USA
fYear :
2003
fDate :
20-22 Nov. 2003
Firstpage :
472
Lastpage :
477
Abstract :
Spacecraft are becoming smaller relative to the amount of scientific information we are acquiring with them. This miniaturization, however, presents even bigger challenges to the spacecraft developers. First, none of these programs have the resources to reinvent the wheel again for their projects. Second, the requirements in communication, operations and software development are not only contained in the transition from bigger satellites to smaller, but sometimes even complicated by this miniaturization.
Keywords :
aerospace testing; artificial satellites; data handling; satellite communication; SSDL; STRING mission; Stanford University Space Systems Development Laboratory; Stanford-TUI Tether Release In Neutral Gravity; Tethers Unlimited Inc.; miniaturization; satellites; scientific information; software development; spacecraft; tether dynamics testing; Aerodynamics; Educational institutions; Electrodynamics; Laboratories; Propulsion; Satellites; Space missions; Space technology; Space vehicles; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies, 2003. RAST '03. International Conference on. Proceedings of
Conference_Location :
Istanbul, Turkey
Print_ISBN :
0-7803-8142-4
Type :
conf
DOI :
10.1109/RAST.2003.1303962
Filename :
1303962
Link To Document :
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