Optimization problems caused by interaction of guidance and propellant systems.Optimization of Saturn vehicle, considering interaction of guidance, control and propellant utilization systems
Document ID
19670041246
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chandler, D. C.
Horn, H. J.
Ryan, R. S.
Date Acquired
August 3, 2013
Publication Date
July 1, 1966
Subject Category
Navigation
Report/Patent Number
AAS PAPER 66-117Report Number: AAS PAPER 66-117
Accession Number
67A19975
Distribution Limits
Public
Copyright
Other
Keywords
GUIDANCE AND CONTROLSATURN LAUNCH VEHICLEOPTIMIZATIONLIQUID PROPELLANT