A typical geosynchronous spacecraft requires 15 m / s / yr for orbital stationkeeping and momentum dumping.
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A typical geosynchronous spacecraft requires 15 m / s / yr for orbital stationkeeping and momentum dumping. The satellite must last 10 years, and has a dry mass of 4000 kg. What is the fuel budget for monopropellant hydrazine with lsp = 220 s?
Related Book For
Vector Mechanics for Engineers Statics and Dynamics
ISBN: 978-0073212227
8th Edition
Authors: Ferdinand Beer, E. Russell Johnston, Jr., Elliot Eisenberg, William Clausen, David Mazurek, Phillip Cornwell
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