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Abort-once-around entry corridor analysis program documentThe abort once around entry target corridor analysis program (ABECAP) was studied. The allowable range of flight path angles at entry interface for acceptable entry trajectories from a shuttle abort once around (AOA) situation was established. The solutions thus determined may be shown as corridor plots of entry interface flight path angle versus range from entry interface (EI) to the target.
Document ID
19760025130
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kyle, H. C.
(McDonnell-Douglas Technical Services Co., Inc. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
December 23, 1975
Subject Category
Astrodynamics
Report/Patent Number
DN-1.4-4-17
NASA-CR-150974
Report Number: DN-1.4-4-17
Report Number: NASA-CR-150974
Accession Number
76N32218
Funding Number(s)
CONTRACT_GRANT: NAS9-13970
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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