NASA NTRS · 19830000632
Elliptical Orbit Performance Computer Program
Abstract
Elliptical 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.
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Myler, T.. 1984-11-01. Elliptical Orbit Performance Computer Program. https://ntrs.nasa.gov/citations/19830000632
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