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Volumn 34, Issue 5, 2004, Pages 1246-1250
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A method of calculating fragment velocity additions for the analysis of the breakup of a launch vehicle upper stage
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Author keywords
Fragment velocity additions; Orbital breakup event; Space debris
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Indexed keywords
DRAG;
ORBITS;
PERTURBATION TECHNIQUES;
SATELLITE OBSERVATORIES;
SPACE DEBRIS;
VELOCITY MEASUREMENT;
ANGULAR MOMENTUM VECTOR;
FRAGMENT VELOCITY ADDITIONS;
LAUNCH VEHICLES;
ORBITAL BREAKUP EVENTS;
CATAPULTS (AIRCRAFT LAUNCHERS);
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EID: 3242729343
PISSN: 02731177
EISSN: None
Source Type: Journal
DOI: 10.1016/j.asr.2003.10.042 Document Type: Conference Paper |
Times cited : (5)
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References (3)
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