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Rocket trajectory optimization by a second- order numerical technique

Authors :
S. S. Mckay
B. R. Uzzell
H. J. Kelley
Source :
AIAA Journal. 7:879-884
Publication Year :
1969
Publisher :
American Institute of Aeronautics and Astronautics (AIAA), 1969.

Abstract

Multistage rocket trajectories optimized by second order numerical technique and digital computer program, considering coasting, vacuum flight and transition times

Subjects

Subjects :
Propellant
Physics
business.product_category
ComputingMilieux_THECOMPUTINGPROFESSION
Eccentric anomaly
business.industry
Numerical analysis
Aerospace Engineering
ComputerApplications_COMPUTERSINOTHERSYSTEMS
Trajectory optimization
Propulsion
GeneralLiterature_MISCELLANEOUS
Multistage rocket
Physics::Geophysics
Numerical integration
Rocket
Aerospace engineering
business

Details

ISSN :
1533385X and 00011452
Volume :
7
Database :
OpenAIRE
Journal :
AIAA Journal
Accession number :
edsair.doi...........d7e909a600044808c321e45a74e479d0

Tools

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