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Ascent trajectory dispersion analysisThe results of a Space Transportation System ascent trajectory dispersion analysis are documented. Critical trajectory parameter values useful for the definition of lightweight external tank insulation requirements are provided. This analysis was conducted using two of the critical missions specified for the Space Transportation System: a 28.5 deg inclination trajectory launched from the Eastern Test Range (ETR) and a Western Test Range (WTR) trajectory launched into a 104 deg orbital inclination.
Document ID
19830016258
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
December 1, 1982
Subject Category
Astrodynamics
Report/Patent Number
NASA-CR-170741
NAS 1.26:170741
TR82-MSFC-34431-048
Report Number: NASA-CR-170741
Report Number: NAS 1.26:170741
Report Number: TR82-MSFC-34431-048
Accession Number
83N24529
Funding Number(s)
CONTRACT_GRANT: NAS8-34431
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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