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Preliminary Characterization of IDCSP Spacecrafts Through a Multi-Analytical ApproachDefining the risks present to both crewed and robotic spacecrafts is part of NASA s mission, and is critical to keep these resources out of harm s way. Characterizing orbital debris is an essential part of this mission. We present a proof-of-concept study that employs multiple techniques to demonstrate the efficacy of each approach. The targets of this study are IDCSPs (Initial Defense Communications Satellite Program). 35 of these satellites were launched by the US in the mid-1960s and were the first US military communications satellites in the GEO regime. They were emplaced in slightly sub-synchronous orbits. These targets were chosen for this proof-of-concept study for the simplicity of their observable exterior surfaces. The satellites are 26-sided polygons (86cm in diameter), initially spin-stabilized, and covered on all sides in solar panels. Data presented here include: (a) visible broadband photometry (Johnson/Kron-Cousins BVRI) taken with the 0.9m SMARTs telescope (Small and Medium Aperture Telescopes) at the Cerro Tololo Inter-American Observatory (CTIO) in Chile in April, 2012, (b) laboratory broadband photometry (Johnson/ Bessell BVRI) of solar cells, obtained using the Optical Measurements Center (OMC) at NASA/JSC [1], (c) visible-band spectra taken using the Magellan 6.5m Baade Telescope at Las Campanas Observatory in Chile in May, 2012 [2], and (d) visible-band laboratory spectra of solar cells using an ASD Field Spectrometer. Color-color plots using broadband photometry (e.g. B-R vs. B-V) demonstrate that different material types fall into distinct areas on the plots [1]. Spectra of the same material types as those plotted in the color-color plots each display their own signature as well. Here, we compare lab data with telescopic data, and photometric results with spectroscopic results. The spectral response of solar cells in the visible wavelength regime varies from relatively flat to somewhat older solar cells whose reflectivity can be gently or sharply peaked in the blue. With a target like IDCSPs, the material type is known a priori, aiding in understanding how material type affects one s observations.
Document ID
20120015712
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Lederer, S. M.
(NASA Johnson Space Center Houston, TX, United States)
Seitzer, P.
(Michigan Univ. Ann Arbor, MI, United States)
Cowardin, H. M.
(Jacobs Engineering Group, Inc. Houston, TX, United States)
Barker, E. S.
(LZ Technology, Inc. Houston, TX, United States)
Abercromby, K. J.
(California State Polytechnic Coll. San Luis Obispo, CA, United States)
Burkhardt, Andrew
(Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
August 26, 2013
Publication Date
September 11, 2012
Subject Category
Space Transportation And Safety
Report/Patent Number
JSC-CN-27060
Report Number: JSC-CN-27060
Distribution Limits
Public
Copyright
Public Use Permitted.
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