DocumentCode :
2068204
Title :
SOCEM: Sub-Orbital CubeSat Experimental Mission
Author :
Lumpp, James E. ; Karam, Anthony K ; Erb, D.M. ; Bratcher, Jason R ; Rawashdeh, Samir A. ; Clements, Twyman ; Fite, Nathan ; Kruth, Jeffrey ; Malphrus, Benjamin ; Bland, I. ; Munakata, Riki ; Coelho, Rui ; Puig-Suari, Jordi ; Reese, Jackson ; Brodell, Cha
Author_Institution :
Univ. of Kentucky, Lexington, KY, USA
fYear :
2010
fDate :
6-13 March 2010
Firstpage :
1
Lastpage :
9
Abstract :
SOCEM: Sub-Orbital CubeSat Experimental Mission will attempt, for the first time, to eject CubeSats in space from a sub-orbital sounding rocket. This technology demonstration flight will eject two CubeSats from a standard 17-inch diameter NASA sounding rocket. Two student-designed and student-built CubeSats will be ejected as part of the mission, a 2U CubeSat ADAMASat (Antenna Deployment and Mono-filament Actuator Satellite) developed by Kentucky Space to test CubeSat actuator designs and a 1U CubeSat developed by Cal Poly as a test-bed for PolySat bus technologies. The CubeSats will be ejected perpendicular to the direction of flight without requiring a de-spin maneuver providing the CubeSats with several minutes in space before re-entry and impact in the Atlantic Ocean. The SOCEM flight is scheduled for launch on 21 January 2010. Success in this effort could provide a robust ride-share technology for future NASA sounding rocket missions.
Keywords :
aerospace instrumentation; aircraft antennas; artificial satellites; rockets; 2U CubeSat ADAMASat; Atlantic Ocean; Cal Poly; Kentucky Space; NASA sounding rocket; PolySat bus technology; SOCEM; Sub-Orbital CubeSat Experimental Mission; antenna deployment; de-spin maneuver; demonstration flight; mono-filament actuator satellite; sub-orbital sounding rocket; Actuators; Marine technology; NASA; Oceans; Robustness; Rockets; Satellite antennas; Space missions; Space technology; Testing;
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.2010.5447021
Filename :
5447021
Link To Document :
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