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Space Active Modular Materials Experiments; SAMMES: Low Earth Orbital Mission Aboard the Space Test Experiments Step-3 Platform
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Abstract
Future satellite systems must survive in the space environment for 5 to 10 years to achieve greater cost effectiveness. Characterization of the orbital space environment and effects on spacecraft systems have received considerable attention recently years. Instrumentation has been developed by Physical Sciences Inc., under Ballistic Missile Defense Office (BMDO) sponsorship, 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. 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.
Authors
- P. Joshi - Physical Sciences Inc.
- D. Palombo - Physical Sciences Inc.
- M. Malonson - Physical Sciences Inc.
- W. Whitehouse - Physical Sciences Inc.
- D. Oakes - Physical Sciences Inc.
- B. D. Green - Physical Sciences Inc.
- V. Di Cristina - Physical Sciences Inc.
- J. McKay - Research Support Instruments
- W. Nicholas - Research Support Instruments
- M. Obal
- D. Brinza
- G. Arnold
- J. Durrett
Citation
Joshi, P., Palombo, D., Malonson, M., Whitehouse, W. et al., "Space Active Modular Materials Experiments; SAMMES: Low Earth Orbital Mission Aboard the Space Test Experiments Step-3 Platform," SAE Technical Paper 951641, 1995, https://doi.org/10.4271/951641.Also In
References
- Richelt P Triolo J Progress in Astronautics and Aeronautics 20 491 513 Academic Press NY 1969