Space Active Modular Materials Experiments (SAMMES): Low Earth Orbital mission aboard the Space Test Experiments STEP-3 platformThe requirement of satellite systems to survive in the space environment for 5 to 10 years to achieve greater cost effectiveness is discussed. Characterization of the orbital space environment and its effects on spacecraft systems have received considerable research attention. Instrumentation for long term measurement of key physical parameters characterizing the low Earth orbit (LEO) environment and its effects on degradation of spacecraft materials and solar arrays is reported. These measurements enable active, real time monitoring of the health of spacecraft and payload systems. SAMMES is designed to be autonomous, compact, low power, and lightweight.
Document ID
19950021163
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Joshi, P. (Physical Sciences, Inc. Andover, MA., United States)
Palombo, D. (Physical Sciences, Inc. Andover, MA., United States)
Malonson, M. (Physical Sciences, Inc. Andover, MA., United States)
Whitehouse, W. (Physical Sciences, Inc. Andover, MA., United States)
Oakes, D. (Physical Sciences, Inc. Andover, MA., United States)
Green, B. D. (Physical Sciences, Inc. Andover, MA., United States)
Dicristina, V. (Physical Sciences, Inc. Andover, MA., United States)
Mckay, J. (Research Support Instruments, Inc. Baltimore, MD., United States)
Nicholas, W. (Research Support Instruments, Inc. Baltimore, MD., United States)
Obal, M. (Ballistic Missile Defense Organization Washington, DC., United States)
Date Acquired
August 16, 2013
Publication Date
November 1, 1994
Publication Information
Publication: ESA, Proceedings of 6th International Symposium on Materials in a Space Environment