This chapter contains sections titled:
Introduction
Keplerian Orbit Transfers
Mission Analysis
Polar LEO/Remote‐Sensing Satellites
Satellite Constellations
Geostationary Earth Orbits (GEO)
Highly Elliptic Orbits
Interplanetary Missions
Mission Analysis
Spacecraft Systems Engineering ; 111-175
2011-08-12
65 pages
Article/Chapter (Book)
Electronic Resource
English
mission analysis ‐ celestial mechanics and spacecraft's dynamics , spacecraft launch time , Keplerian orbit transfers ‐ space vehicle, one orbit to another , mission analysis, ‘front‐end’ systems level activity ‐ and celestial mechanics , two principal constraints ‐ design of aeromanoeuvring vehicle , polar LEO/remote‐sensing satellites , interplanetary missions for interplanetary spacecraft , missions, categories ‐ Low Earth Orbit (LEO), MEO, GEO, HEO and non‐geocentric orbits
NTRS | 1964
|TIBKAT | 2020
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