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Summary of saturn i base thermal environment.Base thermal environment measured on flight tests of eight-engine LOX/RP-1 propelled Saturn I booster
Document ID
19650033907
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jones, I. P., Jr.
Payne, R. G.
Date Acquired
August 2, 2013
Publication Date
February 1, 1965
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 65-212
Report Number: AIAA PAPER 65-212
Accession Number
65A16611
Distribution Limits
Public
Copyright
Other
Keywords
HEAT SHIELD
LOX-HYDROGEN ENGINE
SATURN I LAUNCH VEHICLE
BASE HEATING

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