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Thiokol 260-SL nozzle development programTape wrapped ablative steel jacketed nozzle for 156 and 200 inch diameter solid propellant rocket engines
Document ID
19680007010
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 2, 2013
Publication Date
January 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-54870
SBR-90.865
Report Number: NASA-CR-54870
Report Number: SBR-90.865
Accession Number
68N16479
Funding Number(s)
CONTRACT_GRANT: NAS3-6285
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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