DocumentCode :
2434236
Title :
Structural Bus and Release Mechanisms on the ST5 Satellites - Summary and Status
Author :
Rossoni, Peter
Author_Institution :
NASA Goddard Space Flight Center, Greenbelt
fYear :
2007
fDate :
3-10 March 2007
Firstpage :
1
Lastpage :
14
Abstract :
The Space Technology 5 Mechanical System met the challenge of packaging a fully functional science and technology satellite system with its Deployer mechanism into a compact 0.07 m3 volume. Three 25 kg satellites were orbited in constellation in March, 2006. The ST5 mechanical system is composed of (1) The Structural Bus; (2) Magnetometer Instrument Boom (3) Spacecraft Deployer Release Mechanism. This system includes a highly integrated electronics enclosure as a multifunctional structure; a lightweight, magnetically clean Magnetometer Boom; the first use of Nitinol Shape-Memory Alloy trigger devices for deploying multiple spacecraft; an innovative compliant mount for the umbilical connector and a Deployer mechanism that imparts both separation velocity and mission spin rate to three constellation flying satellites. These elements employed cutting-edge design and analysis tools, state-of-the-art testing facilities and proven engineering techniques to meet stringent performance criteria, enabling the mission´s success.
Keywords :
artificial satellites; Deployer mechanism; ST5 satellites; Space Technology 5 Mechanical System; magnetometer instrument boom; mass 25 kg; release mechanisms; structural bus; Aerospace electronics; Instruments; Magnetic devices; Magnetic separation; Magnetometers; Mechanical systems; Packaging; Satellites; Space technology; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2007 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
1-4244-0524-6
Electronic_ISBN :
1095-323X
Type :
conf
DOI :
10.1109/AERO.2007.352783
Filename :
4161318
Link To Document :
بازگشت