Computer Science – Performance
Scientific paper
Aug 1984
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1984adans..54..443p&link_type=abstract
IN: Astrodynamics 1983; Proceedings of the Conference, Lake Placid, NY, August 22-25, 1983. Part 1 (A84-30526 13-13). San Diego,
Computer Science
Performance
Artificial Satellites, Low Altitude, Performance Prediction, Propellant Combustion, Propellant Storability, Satellite Lifetime, Aerodynamic Drag, Atmospheric Density, Diurnal Variations, Mission Planning, Propellant Mass Ratio, Tradeoffs
Scientific paper
Continuous and discrete forms of the propellant longevity equation are derived. Expressions for the propellant mass decrement equation are developed for both spherically symmetrical and oblate diurnal atmospheres. The result for the oblate diurnal atmosphere is applied to the discrete form of the propellant longevity equation to provide numerical examples illustrating their application to several areas of mission planning.
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