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Elliptical Orbit Performance Computer ProgramElliptical Orbit Performance (ELOPE) computer program for analyzing orbital performance of space boosters uses orbit insertion data obtained from trajectory simulation to generate parametric data on apogee and perigee altitudes as function of payload data. Data used to generate presentation plots that display elliptical orbit performance capability of space booster.
Document ID
19830000632
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Myler, T. (Vought Corp.)
Date Acquired
August 11, 2013
Publication Date
November 1, 1984
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13026
Accession Number
83B10632
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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