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An Attempt to Observe Debris from the Breakup of a Titan 3C-4 TranstageIn February 2007 dedicated observations were made of the orbital space predicted to contain debris from the breakup of the Titan 3C-4 transtage back on February 21, 1992. These observations were carried out on the Michigan Orbital DEbris Survey Telescope (MODEST) in Chile with its 1.3deg field of view. The search region or orbital space (inclination and right ascension of the ascending node (RAAN) was predicted using NASA#s LEGEND (LEO-to-GEO Environment Debris) code to generate a Titan debris cloud. Breakup fragments are created based on the NASA Standard Breakup Model (including fragment size, area-to-mass (A/M), and delta-V distributions). Once fragments are created, they are propagated forward in time with a subroutine GEOPROP. Perturbations included in GEOPROP are those due to solar/lunar gravity, radiation pressure, and major geopotential terms. Barker, et. al, (AMOS Conference Proceedings, 2006, pp. 596-604) used similar LEGEND predictions to correlate survey observations made by MODEST (February 2002) and found several possible night-to-night correlations in the limited survey dataset. One conc lusion of the survey search was to dedicate a MODEST run to observing a GEO region predicted to contain debris fragments and actual Titan debris objects (SSN 25000, 25001 and 30000). Such a dedicated run was undertaken with MODEST between February 17 and 23, 2007 (UT dates). MODEST#s limiting magnitude of 18.0 (S\N approx.10) corresponds to a size of 22cm assuming a diffuse Lambertian albedo of 0.2. However, based on observed break-up data, we expect most debris fragments to be smaller than 22cm which implies a need to increase the effective sensitivity of MODEST for smaller objects. MODEST#s limiting size can be lowered by increasing the exposure time (20 instead of 5 seconds) and applying special image processing. The special processing combines individual CCD images to detect faint objects that are invisible on a single CCD image. Sub-images are cropped from six consecutive CCD images with pixel shifts between images being consistent with the predicted movement of a Titan object. A median image of all the sub-images is then created leaving only those objects with the proper Titan motion. Limiting the median image in this manner brings the needed computer time to process all images taken on one night down to about 50 hours of CPU time.
Document ID
20070018026
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Barker, E. S.
(NASA Johnson Space Center Houston, TX, United States)
Matney, M. J.
(NASA Johnson Space Center Houston, TX, United States)
Yanagisawa, T.
(Japan Aerospace Exploration Agency Tokyo, Japan)
Liou, J.-C.
(Jacobs Sverdrup Technology, Inc. Houston, TX, United States)
Abercromby, K. J.
(Jacobs Sverdrup Technology, Inc. Houston, TX, United States)
Rodriquez, H. M.
(Jacobs Sverdrup Technology, Inc. Houston, TX, United States)
Horstman, M. F.
(Jacobs Sverdrup Technology, Inc. Houston, TX, United States)
Seitzer, P.
(Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2007
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 2007 AMOS Technical Conference
Location: Maui, HI
Country: United States
Start Date: September 12, 2007
End Date: September 15, 2007
Sponsors: Maui Economic Development Board
Distribution Limits
Public
Copyright
Public Use Permitted.
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