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STS-9 BET productsThe final products generated for the STS-9, which landed on December 8, 1983 are reported. The trajectory reconstruction utilized an anchor epoch of GMT corresponding to an initial altitude of h 356 kft, selected in view of the limited tracking coverage available. The final state utilized IMU2 measurements and was based on processing radar tracking from six C-bands and a single S-band station, plus six photo-theodolite cameras in the vicinity of Runway 17 at Edwards Air Force Base. The final atmosphere (FLAIR9/UN=581199C) was based on a composite of the remote measured data and the 1978 Air Force Reference Atmosphere model. The Extended BET is available as STS9BET/UN=274885C. The AEROBET and MMLE input files created are discussed. Plots of the more relevant parameters from the AEROBET (reel number NL0624) are included. Input parameters, final residual plots, a trajectory listing, and data archival information are defined.
Document ID
19840012548
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Findlay, J. T.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Kelly, G. M.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Heck, M. L.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Mcconnell, J. G.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Henry, M. W.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1984
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-172314
NAS 1.26:172314
AMA-84-3
Report Number: NASA-CR-172314
Report Number: NAS 1.26:172314
Report Number: AMA-84-3
Accession Number
84N20616
Funding Number(s)
CONTRACT_GRANT: NAS1-16087
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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