NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
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
19660048583
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Jones, I. P.
Payne, R. G.
Date Acquired
August 3, 2013
Publication Date
April 1, 1966
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 65-212
Report Number: AIAA PAPER 65-212
Accession Number
66A27873
Distribution Limits
Public
Copyright
Other
Keywords
SATURN I LAUNCH VEHICLE
BASE HEATING
LOX-HYDROGEN ENGINE
HEAT SHIELD

Available Downloads

There are no available downloads for this record.
No Preview Available