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A TECHNIQUE FOR OPTIMIZATION OF ASCENT TRAJECTORIES AND PROPELLANT LOADINGS OF MULTISTAGE SPACE VEHICLESVariational calculus and computer logic for optimization of ascent trajectories and propellant loadings of multistage space vehicles
Document ID
19630023439
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Thomae, H. F.
Date Acquired
August 1, 2013
Publication Date
May 24, 1963
Subject Category
Space Radiation
Report/Patent Number
DGRR PAPER 1535 /63/
Report Number: DGRR PAPER 1535 /63/
Accession Number
63A19498
Distribution Limits
Public
Copyright
Other
Keywords
MULTISTAGE VEHICLE
COMPUTER PROGRAM
TRAJECTORY
VARIATIONAL CALCULUS

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