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Volumn , Issue , 2004, Pages 9815-9821
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Generalized vehicle performance closure model for two-stage-to-orbit launch vehicles
a b a c d |
Author keywords
[No Author keywords available]
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Indexed keywords
ADVANCED ENGINEERING ENVIRONMENT (AEE);
NEXT GENERATION LAUNCH TECHNOLOGIES (NGLT);
PRODUCT DATA MANAGEMENT (PDM) SYSTEM;
TWO-STAGE-TO-ORBIT (TSTO) LAUCH VEHICLES;
AERODYNAMICS;
BOOSTERS (ROCKET);
CATAPULTS (AIRCRAFT LAUNCHERS);
COMPUTATIONAL GEOMETRY;
COMPUTER AIDED DESIGN;
COMPUTER PROGRAMMING LANGUAGES;
DATA ACQUISITION;
MATHEMATICAL MODELS;
ORBITS;
PARAMETER ESTIMATION;
PLANNING;
PROPELLANTS;
XML;
AEROSPACE ENGINEERING;
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EID: 2942718894
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (2)
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References (9)
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