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Dispersion analysis for baseline reference mission 2A dispersion analysis considering uncertainties (or perturbations) in platform, vehicle, and environmental parameters was performed for baseline reference mission (BRM) 2. The dispersion analysis is based on the nominal trajectory for BRM 2. The analysis was performed to determine state vector and performance dispersions (or variations) which result from the indicated uncertainties. The dispersions are determined at major mission events and fixed times from liftoff (time slices). The dispersion results will be used to evaluate the capability of the vehicle to perform the mission within a specified level of confidence and to determine flight performance reserves.
Document ID
19760026151
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Snow, L. S.
(McDonnell-Douglas Technical Services Co., Inc. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
November 14, 1975
Subject Category
Astrodynamics
Report/Patent Number
NASA-CR-151021
DN-1.4-7-18
Report Number: NASA-CR-151021
Report Number: DN-1.4-7-18
Accession Number
76N33239
Funding Number(s)
CONTRACT_GRANT: NAS9-13970
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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