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Nanosatellite Launch Adapter System (NLAS)The utility of small spacecraft based on the University cubesat standard is becoming evident as more and more agencies and organizations are launching or planning to include nanosatellites in their mission portfolios. Cubesats are typically launched as secondary spacecraft in enclosed, containerized deployers such as the CalPoly Poly Picosat Orbital Deployer (P-POD) system. The P-POD allows for ease of integration and significantly reduces the risk exposure to the primary spacecraft and mission. NASA/ARC and the Operationally Responsive Space office are collaborating to develop a Nanosatellite Launch Adapter System (NLAS), which can accommodate multiple cubesat or cubesat-derived spacecraft on a single launch vehicle. NLAS is composed of the adapter structure, P-POD or similar spacecraft dispensers, and a sequencer/deployer system. This paper describes the NLAS system and it s future capabilities, and also provides status on the system s development and potential first use in space.
Document ID
20100033805
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Yost, Bruce D.
(NASA Ames Research Center Moffett Field, CA, United States)
Hines, John W.
(NASA Ames Research Center Moffett Field, CA, United States)
Agasid, Elwood F.
(NASA Ames Research Center Moffett Field, CA, United States)
Buckley, Steven J.
(Department of Defense Kirtland AFB, NM, United States)
Date Acquired
August 25, 2013
Publication Date
March 8, 2010
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN1284
AIAA Paper RS8-2010-5004
Report Number: ARC-E-DAA-TN1284
Report Number: AIAA Paper RS8-2010-5004
Meeting Information
Meeting: Responsive Space 8
Location: Los Angeles, CA
Country: United States
Start Date: March 8, 2010
End Date: March 11, 2010
Distribution Limits
Public
Copyright
Public Use Permitted.
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