DocumentCode
1878278
Title
Integration and management challenges for multi-nanosatellite missions
Author
Kanter, Matthew H. ; Sedam, Kitty J.
Author_Institution
Space Innovation Directorate, Aerosp. Corp., Kirtland AFB, NM, USA
fYear
2012
fDate
3-10 March 2012
Firstpage
1
Lastpage
8
Abstract
The need for launch opportunities for nanosatellite missions is ever increasing as the number of nanosatellites in development increases. Nanosatellites are typically launched as secondary, also known as auxiliary payloads, on missions to minimize launch costs. This creates managerial and technical challenges for integrating multiple nanosatellite programs as auxiliary payloads with primary missions. The priority of the integration team is to minimize impacts and risks to the primary spacecraft and the launch vehicle that are present with auxiliary satellites. Early identification of requirements for nanosatellites and their deployment devices is necessary to increase the opportunity for success of a nanosatellite rideshare mission. This paper discusses management and integration challenges for nanosatellite missions that are launched as auxiliary payloads on United States launch vehicles and techniques for addressing these challenges.
Keywords
artificial satellites; space vehicles; United States launch vehicles; auxiliary payloads; multinanosatellite mission; spacecraft; Payloads; Safety; Satellites; Space vehicles; Standards; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2012 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4577-0556-4
Type
conf
DOI
10.1109/AERO.2012.6187007
Filename
6187007
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