A variational method for multistage launch vehicle optimization.Calculus of variations method used to maximize payload capability for multistage launch vehicles
Document ID
19660039708
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Spurlock, O. F.
Teren, F.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 66-92Report Number: AIAA PAPER 66-92
Accession Number
66A18998
Distribution Limits
Public
Copyright
Other
Keywords
PAYLOAD MASS RATIOMULTISTAGE ROCKET VEHICLEVARIATIONAL CALCULUS