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Theoretical and experimental investigation of heating from Saturn solid propellant rocket exhausts.Heating from Saturn solid propellant S-II and S-IVB ullage motor exhausts and S-IB, S-IVB and Centaur retro motor exhaust theoretically and experimentally analyzed
Document ID
19660057310
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rochelle, W. C.
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 66-653
Report Number: AIAA PAPER 66-653
Accession Number
66A36600
Distribution Limits
Public
Copyright
Other
Keywords
EXHAUST NOZZLE
SATURN LAUNCH VEHICLE
SOLID PROPELLANT ROCKET ENGINE
ROCKET EXHAUST

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