DocumentCode
2061574
Title
Colloid Micro-Newton Thrusters for the space technology 7 mission
Author
Ziemer, John K. ; Randolph, Thomas M. ; Franklin, Garth W. ; Hruby, Vlad ; Spence, Douglas ; Demmons, Nathaniel ; Roy, Thomas ; Ehrbar, Eric ; Zwahlen, Jurg ; Martin, Roy ; Connolly, William
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
2010
fDate
6-13 March 2010
Firstpage
1
Lastpage
19
Abstract
Two flight-qualified clusters of four Colloid Micro-Newton Thruster (CMNT) systems have been delivered to the Jet Propulsion Laboratory (JPL) and subsequently delivered to ESA for spacecraft integration. The clusters will provide precise spacecraft control for the drag-free technology demonstration mission, Space Technology 7 (ST7). The ST7 mission is sponsored by the NASA New Millennium Program and will demonstrate precision formation flying technologies for future missions such as the Laser Interferometer Space Antenna (LISA) mission. The ST7 disturbance reduction system (DRS) is a payload on the ESA LISA Pathfinder spacecraft along with the European gravitational reference sensor (GRS) as part of the ESA LISA Technology Package (LTP). To achieve the nanometer-level precision spacecraft control requirements, each of eight thruster systems is required to provide thrust between 5 and 30 ?N with resolution ?0.1 ?N and thrust noise ?0.1 ?N/?(Hz). Developed by Busek Co. Inc., with support from JPL in design and testing, the CMNT has been developed over the last six years into a flight-ready and flight-qualified microthruster system, the first of its kind. Recent flight-unit qualification tests have included vibration and thermal vacuum environmental testing, as well as performance verification and acceptance tests. All tests have been completed successfully prior to delivery to JPL. Delivery of the first flight unit occurred in February of 2008 with the second unit following in May of 2008. Since arrival at JPL, the units have successfully passed through mass distribution, magnetic, and EMI/EMC measurements and tests as part of the integration and test (I&T) activities including the integrated avionics unit (IAU). Flight software sequences have been tested and validated with the full flight DRS instrument successfully to the extent possible in ground testing, including full functional and 72 hour autonomous operations tests. In the summer of 2009 the cluster assem- - blies were delivered to ESA along with the IAU for integration into the LISA Pathfinder spacecraft. Spacecraft-level testing will include magnetics, acoustic, and thermal vacuum environmental testing with a planned launch and flight demonstration in April 2012.
Keywords
aerospace control; aerospace propulsion; aerospace testing; avionics; position control; space vehicles; EMI/EMC measurements; ESA LISA Pathfinder spacecraft; ESA LISA technology package; European gravitational reference sensor; Jet Propulsion Laboratory; NASA New Millennium Program; ST7 disturbance reduction system; Space Technology 7 mission; acceptance tests; colloid micro-Newton thrusters; drag-free technology; flight software sequences; flight-qualified microthruster system; flight-unit qualification tests; formation flying technologies; integrated avionics unit; laser interferometer space antenna; mass distribution; nanometer-level precision spacecraft control; performance verification; spacecraft integration; thermal vacuum environmental testing; vibration environmental testing; Acoustic testing; Aerospace electronics; Laboratories; NASA; Payloads; Propulsion; Software testing; Space missions; Space technology; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2010 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-3887-7
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2010.5446760
Filename
5446760
Link To Document